Virtual transponder utilizing inband commanding

ABSTRACT

Systems, methods, and apparatus for a virtual transponder utilizing inband commanding are disclosed. A disclosed method comprises transmitting, by a hosted payload (HoP) operation center (HOC), encrypted hosted commands to a hosted receiving antenna. The method further comprises transmitting, by the hosted receiving antenna, the encrypted hosted commands to a payload antenna on a vehicle. Also, the method comprises transmitting, by a host spacecraft operations center (SOC), encrypted host commands to the vehicle. Additionally, the method comprises reconfiguring a payload on the vehicle according to unencrypted host commands and/or unencrypted hosted commands. In addition, the method comprises transmitting, by the payload antenna, payload data to a host receiving antenna and/or hosted receiving antenna. Also, the method comprises transmitting encrypted host telemetry to the host SOC, and transmitting encrypted hosted telemetry to the host SOC. Further, the method comprises transmitting, by the host SOC, the encrypted hosted telemetry to the HOC.

FIELD

The present disclosure relates to virtual transponders. In particular,it relates to virtual transponders utilizing inband commanding.

BACKGROUND

Currently, typical transponders on a vehicle (e.g., a satellite) havethe ability to perform switching of inputs to outputs of the payload.All of this switching on the payload is commanded and controlled by asingle satellite controller with no resource allocation privacy. Forexample, in a digital transponder, when a user request for a channelwith specific bandwidth and antenna characteristics is made, the channelis then set up, used, and then disconnected.

As such, there is a need for an improved transponder design that allowsfor privacy in the allocation of resources on the payload.

SUMMARY

The present disclosure relates to a method, system, and apparatus forvirtual transponders utilizing inband commanding. In one or moreembodiments, a method for a virtual transponder utilizing inbandcommanding comprises transmitting, by a hosted payload (HoP) operationcenter (HOC), encrypted hosted commands to a hosted receiving antenna,where the encrypted hosted commands are encrypted utilizing a secondcommunication security (COMSEC) variety. The method further comprisestransmitting, by the hosted receiving antenna, the encrypted hostedcommands to a payload antenna on a vehicle. Also, the method comprisestransmitting, by a host spacecraft operations center (SOC), encryptedhost commands to the vehicle, where the encrypted host commands areencrypted utilizing a first COMSEC variety. In addition, the methodcomprises decrypting, by a first communication security module, theencrypted host commands utilizing the first COMSEC variety to generateunencrypted host commands. Additionally, the method comprisesdecrypting, by a second communication security module, the encryptedhosted commands utilizing the second COMSEC variety to generateunencrypted hosted commands. Also, the method comprises reconfiguring apayload on the vehicle according to the unencrypted host commands and/orthe unencrypted hosted commands. Additionally, the method comprisestransmitting, by the payload antenna, payload data to a host receivingantenna and/or the hosted receiving antenna. Also, the method comprisesencrypting, by the first communication security module, unencrypted hosttelemetry utilizing the first COMSEC variety to generate encrypted hosttelemetry. Additionally, the method comprises encrypting, by the secondcommunication security module, unencrypted hosted telemetry utilizingthe second COMSEC variety to generate encrypted hosted telemetry. Inaddition, the method comprises transmitting, by a host telemetrytransmitter, the encrypted host telemetry to the host SOC. Also, themethod comprises transmitting, by a hosted telemetry transmitter, theencrypted hosted telemetry to the host SOC. Further, the methodcomprises transmitting, by the host SOC, the encrypted hosted telemetryto the HOC.

In one or more embodiments, the reconfiguring of the payload accordingto the unencrypted host commands and/or the unencrypted hosted commandscomprises adjusting at least one of: transponder power, transponderspectrum monitoring, transponder connectivity, transponder gainsettings, transponder limiter settings, transponder automatic levelcontrol settings, transponder phase settings, internal gain generation,bandwidth for at least one beam, at least one frequency band for atleast one of the at least one beam, transponder beamforming settings,effective isotropic radiation power (EIRP) for at least one of the atleast one beam, transponder channels, and/or beam steering.

In at least one embodiment, the reconfiguring of the payload accordingto the unencrypted host commands and/or the unencrypted hosted commandscomprises reconfiguring at least one of: at least one antenna, at leastone analog-to-digital converter, at least one digital-to-analogconverter, at least one beamformer, at least one digital channelizer, atleast one demodulator, at least one modulator, at least one digitalswitch matrix, at least one digital combiner, and/or at least one analogswitch matrix.

In one or more embodiments, the vehicle is an airborne vehicle. In someembodiments, the airborne vehicle is a satellite, aircraft, unmannedaerial vehicle (UAV), or space plane.

In at least one embodiment, a method for a virtual transponder utilizinginband commanding comprises transmitting, by a hosted payload (HoP)operation center (HOC), encrypted hosted commands to a host spacecraftoperations center (SOC), where the encrypted hosted commands areencrypted utilizing a second communication security (COMSEC) variety.The method further comprises transmitting, by the host SOC, theencrypted hosted commands to a vehicle. Also, the method comprisestransmitting, by the host SOC, encrypted host commands to a hostreceiving antenna, where the encrypted host commands are encryptedutilizing a first COMSEC variety. In addition, the method comprisestransmitting, by the host receiving antenna, the encrypted host commandsto a payload antenna on the vehicle. Additionally, the method comprisesdecrypting, by a first communication security module, the encrypted hostcommands utilizing the first COMSEC variety to generate unencrypted hostcommands. Also, the method comprises decrypting, by a secondcommunication security module, the encrypted hosted commands utilizingthe second COMSEC variety to generate unencrypted hosted commands. Inaddition, the method comprises reconfiguring a payload on the vehicleaccording to the unencrypted host commands and/or the unencrypted hostedcommands. Additionally, the method comprises transmitting, by thepayload antenna, payload data to the host receiving antenna and/or ahosted receiving antenna. Also, the method comprises encrypting, by thefirst communication security module, unencrypted host telemetryutilizing the first COMSEC variety to generate encrypted host telemetry.In addition, the method comprises encrypting, by the secondcommunication security module, unencrypted hosted telemetry utilizingthe second COMSEC variety to generate encrypted hosted telemetry.Additionally, the method comprises transmitting, by a host telemetrytransmitter, the encrypted host telemetry to the host SOC. Also, themethod comprises transmitting, by a hosted telemetry transmitter, theencrypted hosted telemetry to the host SOC. Further, the methodcomprises transmitting, by the host SOC, the encrypted hosted telemetryto the HOC.

In one or more embodiments, a method for a virtual transponder utilizinginband commanding comprises transmitting, by a hosted payload (HoP)operation center (HOC), encrypted hosted commands to a hosted receivingantenna, where the encrypted hosted commands are encrypted utilizing asecond communication security (COMSEC) variety. The method furthercomprises transmitting, by the hosted receiving antenna, the encryptedhosted commands to a payload antenna on a vehicle. Also, the methodcomprises transmitting, by a host spacecraft operations center (SOC),encrypted host commands to a host receiving antenna, where the encryptedhost commands are encrypted utilizing a first COMSEC variety. Inaddition, the method comprises transmitting, by the host receivingantenna, the encrypted host commands to a payload antenna on thevehicle. Additionally, the method comprises decrypting, by a firstcommunication security module, the encrypted host commands utilizing thefirst COMSEC variety to generate unencrypted host commands. Also, themethod comprises decrypting, by a second communication security module,the encrypted hosted commands utilizing the second COMSEC variety togenerate unencrypted hosted commands. In addition, the method comprisesreconfiguring a payload on the vehicle according to the unencrypted hostcommands and/or the unencrypted hosted commands. Also, the methodcomprises transmitting, by the payload antenna, payload data to the hostreceiving antenna and/or the hosted receiving antenna. In addition, themethod comprises encrypting, by the first communication security module,unencrypted host telemetry utilizing the first COMSEC variety togenerate encrypted host telemetry. Additionally, the method comprisesencrypting, by the second communication security module, unencryptedhosted telemetry utilizing the second COMSEC variety to generateencrypted hosted telemetry. Also, the method comprises transmitting, bya host telemetry transmitter, the encrypted host telemetry to the hostSOC. In addition, the method comprises transmitting, by a hostedtelemetry transmitter, the encrypted hosted telemetry to the host SOC.Further, the method comprises transmitting, by the host SOC, theencrypted hosted telemetry to the HOC.

In at least one embodiment, a method for a virtual transponder utilizinginband commanding comprises transmitting, by a hosted payload (HoP)operation center (HOC), encrypted hosted commands to a hosted receivingantenna, where the encrypted hosted commands are encrypted utilizing asecond communication security (COMSEC) variety. The method furthercomprises transmitting, by the hosted receiving antenna, the encryptedhosted commands to a payload antenna on a vehicle. Also, the methodcomprises transmitting, by a host spacecraft operations center (SOC),encrypted host commands to a host receiving antenna, where the encryptedhost commands are encrypted utilizing a first COMSEC variety. Inaddition, the method comprises transmitting, by the host receivingantenna, the encrypted host commands to the payload antenna on thevehicle. Additionally, the method comprises decrypting, by a firstcommunication security module, the encrypted host commands utilizing thefirst COMSEC variety to generate unencrypted host commands. Also, themethod comprises decrypting, by a second communication security module,the encrypted hosted commands utilizing the second COMSEC variety togenerate unencrypted hosted commands. In addition, the method comprisesreconfiguring a payload on the vehicle according to the unencrypted hostcommands and/or the unencrypted hosted commands. Additionally, themethod comprises transmitting, by the payload antenna, payload data tothe host receiving antenna and/or the hosted receiving antenna. Also,the method comprises encrypting, by the first communication securitymodule, unencrypted telemetry utilizing the first COMSEC variety togenerate encrypted telemetry. In addition, the method comprisestransmitting, by a telemetry transmitter, the encrypted telemetry to thehost SOC. Further, the method comprises transmitting, by the host SOC,the encrypted telemetry to the HOC.

In one or more embodiments, a method for a virtual transponder utilizinginband commanding comprises transmitting, by a hosted payload (HoP)operation center (HOC), encrypted hosted commands to a hosted receivingantenna, where the encrypted hosted commands are encrypted utilizing asecond communication security (COMSEC) variety. The method furthercomprises transmitting, by the hosted receiving antenna, the encryptedhosted commands to a payload antenna on a vehicle. Also, the methodcomprises transmitting, by a host spacecraft operations center (SOC),the encrypted host commands to a host receiving antenna, where theencrypted host commands are encrypted utilizing a first COMSEC variety.In addition, the method comprises transmitting, by the host receivingantenna, the encrypted host commands to the payload antenna.Additionally, the method comprises decrypting, by a first communicationsecurity module, the encrypted host commands utilizing the first COMSECvariety to generate unencrypted host commands. Also, the methodcomprises decrypting, by a second communication security module, theencrypted hosted commands utilizing the second COMSEC variety togenerate unencrypted hosted commands. In addition, the method comprisesreconfiguring a payload on the vehicle according to the unencrypted hostcommands and/or the unencrypted hosted commands. Additionally, themethod comprises transmitting, by the payload antenna, payload data tothe host receiving antenna and/or the hosted receiving antenna. Also,the method comprises encrypting, by the first communication securitymodule, unencrypted host telemetry utilizing the first COMSEC variety togenerate encrypted host telemetry. In addition, the method comprisesencrypting, by the second communication security module, unencryptedhosted telemetry utilizing the second COMSEC variety to generateencrypted hosted telemetry. Additionally, the method comprisestransmitting, by the payload antenna, the encrypted host telemetry tothe host receiving antenna. Also, the method comprises transmitting, bythe host receiving antenna, the encrypted host telemetry to the hostSOC. In addition, the method comprises transmitting, by the payloadantenna, the encrypted hosted telemetry to the hosted receiving antenna.Further, the method comprises transmitting, by the hosted receivingantenna, the encrypted hosted telemetry to the HOC.

In at least one embodiment, a method for a virtual transponder utilizinginband commanding comprises transmitting, by a hosted payload (HoP)operation center (HOC), encrypted hosted commands to a hosted receivingantenna, where the encrypted hosted commands are encrypted utilizing asecond communication security (COMSEC) variety. The method furthercomprises transmitting, by the hosted receiving antenna, the encryptedhosted commands to a payload antenna on a vehicle. Also, the methodcomprises transmitting, by a host spacecraft operations center (SOC),encrypted host commands to a host receiving antenna, where the encryptedhost commands are encrypted utilizing a first COMSEC variety. Inaddition, the method comprises transmitting, by the host receivingantenna, the encrypted host commands to the payload antenna.Additionally, the method comprises decrypting, by a first communicationsecurity module, the encrypted host commands utilizing the first COMSECvariety to generate unencrypted host commands. Also, the methodcomprises decrypting, by a second communication security module, theencrypted hosted commands utilizing the second COMSEC variety togenerate unencrypted hosted commands. In addition, the method comprisesreconfiguring a payload on the vehicle according to the unencrypted hostcommands and/or the unencrypted hosted commands. Additionally, themethod comprises transmitting, by the payload antenna, payload data tothe host receiving antenna and/or the hosted receiving antenna. Also,the method comprises encrypting, by the first communication securitymodule, unencrypted telemetry utilizing the first COMSEC variety togenerate encrypted telemetry. In addition, the method comprisestransmitting, by the payload antenna, the encrypted telemetry to thehost receiving antenna. Additionally, the method comprises transmitting,by the host receiving antenna, the encrypted telemetry to the host SOC.Also, the method comprises transmitting, by the payload antenna, theencrypted telemetry to the hosted receiving antenna. Further, the methodcomprises transmitting, by the hosted receiving antenna, the encryptedtelemetry to the HOC.

In one or more embodiments, a method for a virtual transponder utilizinginband commanding comprises transmitting, by a hosted payload (HoP)operation center (HOC), encrypted hosted commands to a host spacecraftoperations center (SOC). In one or more embodiments, the encryptedhosted commands are encrypted utilizing a second communication security(COMSEC) variety. The method further comprises transmitting, by the hostSOC, encrypted host commands and the encrypted hosted commands to a hostreceiving antenna. In one or more embodiments, the encrypted hostcommands are encrypted utilizing a first COMSEC variety. Also, themethod comprises transmitting, by the host receiving antenna, theencrypted host commands and the encrypted hosted commands to a payloadantenna on the vehicle. In addition, the method comprises decrypting, bya first communication security module, the encrypted host commandsutilizing the first COMSEC variety to generate unencrypted hostcommands. Additionally, the method comprises decrypting, by a secondcommunication security module, the encrypted hosted commands utilizingthe second COMSEC variety to generate unencrypted hosted commands. Also,the method comprises reconfiguring a payload on the vehicle according toat least one of the unencrypted host commands or the unencrypted hostedcommands. In addition, the method comprises transmitting, by the payloadantenna, payload data to at least one of the host receiving antenna or ahosted receiving antenna. Also, the method comprises encrypting, by thefirst communication security module, unencrypted host telemetryutilizing the first COMSEC variety to generate encrypted host telemetry.In addition, the method comprises encrypting, by the secondcommunication security module, unencrypted hosted telemetry utilizingthe second COMSEC variety to generate encrypted hosted telemetry. Also,the method comprises transmitting, by a host telemetry transmitter, theencrypted host telemetry to the host SOC. In addition, the methodcomprises transmitting, by a hosted telemetry transmitter, the encryptedhosted telemetry to the host SOC. Further, the method comprisestransmitting, by the host SOC, the encrypted hosted telemetry to theHOC.

In one or more embodiments, a system for a virtual transponder utilizinginband commanding comprises a hosted payload (HoP) operation center(HOC) to transmit encrypted hosted commands to a hosted receivingantenna, where the encrypted hosted commands are encrypted utilizing asecond communication security (COMSEC) variety. The system furthercomprises the hosted receiving antenna to transmit the encrypted hostedcommands to a payload antenna on a vehicle. Also, the system comprises ahost spacecraft operations center (SOC) to transmit encrypted hostcommands to the vehicle, where the encrypted host commands are encryptedutilizing a first COMSEC variety. In addition, the system comprises afirst communication security module to decrypt the encrypted hostcommands utilizing the first COMSEC variety to generate unencrypted hostcommands. Additionally, the system comprises a second communicationsecurity module to decrypt the encrypted hosted commands utilizing thesecond COMSEC variety to generate unencrypted hosted commands. Also, thesystem comprises a payload on the vehicle reconfigured according to theunencrypted host commands and/or the unencrypted hosted commands. Inaddition, the system comprises the payload antenna to transmit payloaddata to a host receiving antenna and/or the hosted receiving antenna.Additionally, the system comprises the first communication securitymodule to encrypt unencrypted host telemetry utilizing the first COMSECvariety to generate encrypted host telemetry. Also, the system comprisesthe second communication security module to encrypt unencrypted hostedtelemetry utilizing the second COMSEC variety to generate encryptedhosted telemetry. In addition, the system comprises a host telemetrytransmitter to transmit the encrypted host telemetry to the host SOC.Additionally, the system comprises a hosted telemetry transmitter totransmit the encrypted hosted telemetry to the host SOC. Further, thesystem comprises the host SOC to transmit the encrypted hosted telemetryto the HOC.

In at least one embodiment, a system for a virtual transponder utilizinginband commanding comprises a hosted payload (HoP) operation center(HOC) to transmit encrypted hosted commands to a host spacecraftoperations center (SOC), where the encrypted hosted commands areencrypted utilizing a second communication security (COMSEC) variety.The system further comprises the host SOC to transmit the encryptedhosted commands to a vehicle. Also, the system comprises the host SOC totransmit encrypted host commands to a host receiving antenna, where theencrypted host commands are encrypted utilizing a first COMSEC variety.In addition, the system comprises the host receiving antenna to transmitthe encrypted host commands to a payload antenna on the vehicle.Additionally, the system comprises a first communication security moduleto decrypt the encrypted host commands utilizing the first COMSECvariety to generate unencrypted host commands. Also, the systemcomprises a second communication security module to decrypt theencrypted hosted commands utilizing the second COMSEC variety togenerate unencrypted hosted commands. In addition, the system comprisesa payload on the vehicle reconfigured according to the unencrypted hostcommands and/or the unencrypted hosted commands. Additionally, thesystem comprises the payload antenna to transmit payload data to thehost receiving antenna and/or a hosted receiving antenna. Also, thesystem comprises the first communication security module to encryptunencrypted host telemetry utilizing the first COMSEC variety togenerate encrypted host telemetry. In addition, the system comprises thesecond communication security module to encrypt unencrypted hostedtelemetry utilizing the second COMSEC variety to generate encryptedhosted telemetry. Additionally, the system comprises a host telemetrytransmitter to transmit the encrypted host telemetry to the host SOC.Also, the system comprises a hosted telemetry transmitter to transmitthe encrypted hosted telemetry to the host SOC. Further, the systemcomprises the host SOC to transmit the encrypted hosted telemetry to theHOC.

In one or more embodiments, a system for a virtual transponder utilizinginband commanding comprises a hosted payload (HoP) operation center(HOC) to transmit encrypted hosted commands to a hosted receivingantenna, where the encrypted hosted commands are encrypted utilizing asecond communication security (COMSEC) variety. The system furthercomprises the hosted receiving antenna to transmit the encrypted hostedcommands to a payload antenna on a vehicle. Also, the system comprises ahost spacecraft operations center (SOC) to transmit encrypted hostcommands to a host receiving antenna, where the encrypted host commandsare encrypted utilizing a first COMSEC variety. In addition, the systemcomprises the host receiving antenna to transmit the encrypted hostcommands to a payload antenna on the vehicle. Additionally, the systemcomprises a first communication security module to decrypt the encryptedhost commands utilizing the first COMSEC variety to generate unencryptedhost commands. Also, the system comprises a second communicationsecurity module to decrypt the encrypted hosted commands utilizing thesecond COMSEC variety to generate unencrypted hosted commands. Inaddition, the system comprises a payload on the vehicle reconfiguredaccording to the unencrypted host commands and/or the unencrypted hostedcommands. Additionally, the system comprises the payload antenna totransmit payload data to the host receiving antenna and/or the hostedreceiving antenna. Also, the system comprises the first communicationsecurity module to encrypt unencrypted host telemetry utilizing thefirst COMSEC variety to generate encrypted host telemetry. In addition,the system comprises the second communication security module to encryptunencrypted hosted telemetry utilizing the second COMSEC variety togenerate encrypted hosted telemetry. Additionally, the system comprisesa host telemetry transmitter to transmit the encrypted host telemetry tothe host SOC. Also, the system comprises a hosted telemetry transmitterto transmit the encrypted hosted telemetry to the host SOC. Further, thesystem comprises the host SOC to transmit the encrypted hosted telemetryto the HOC.

In at least one embodiment, a system for a virtual transponder utilizinginband commanding comprises a hosted payload (HoP) operation center(HOC) to transmit encrypted hosted commands to a hosted receivingantenna, where the encrypted hosted commands are encrypted utilizing asecond communication security (COMSEC) variety. The system furthercomprises the hosted receiving antenna to transmit the encrypted hostedcommands to a payload antenna on a vehicle. Also, the system comprises ahost spacecraft operations center (SOC) to transmit encrypted hostcommands to a host receiving antenna, where the encrypted host commandsare encrypted utilizing a first COMSEC variety. In addition, the systemcomprises the host receiving antenna to transmit the encrypted hostcommands to the payload antenna on the vehicle. Additionally, the systemcomprises a first communication security module to decrypt the encryptedhost commands utilizing the first COMSEC variety to generate unencryptedhost commands. Also, the system comprises a second communicationsecurity module to decrypt the encrypted hosted commands utilizing thesecond COMSEC variety to generate unencrypted hosted commands. Inaddition, the system comprises a payload on the vehicle reconfiguredaccording to the unencrypted host commands and/or the unencrypted hostedcommands. Additionally, the system comprises transmitting, by thepayload antenna, payload data to the host receiving antenna and/or thehosted receiving antenna. Also, the system comprises the firstcommunication security module to encrypt unencrypted telemetry utilizingthe first COMSEC variety to generate encrypted telemetry. In addition,the system comprises a telemetry transmitter to transmit the encryptedtelemetry to the host SOC. Further, the system comprises the host SOC totransmit the encrypted telemetry to the HOC.

In one or more embodiments, a system for a virtual transponder utilizinginband commanding comprises a hosted payload (HoP) operation center(HOC) to transmit encrypted hosted commands to a hosted receivingantenna, where the encrypted hosted commands are encrypted utilizing asecond communication security (COMSEC) variety. The system furthercomprises the hosted receiving antenna to transmit the encrypted hostedcommands to a payload antenna on a vehicle. Also, the system comprises ahost spacecraft operations center (SOC) to transmit the encrypted hostcommands to a host receiving antenna, where the encrypted host commandsare encrypted utilizing a first COMSEC variety. In addition, the systemcomprises the host receiving antenna to transmit the encrypted hostcommands to the payload antenna. Additionally, the system comprises afirst communication security module to decrypt the encrypted hostcommands utilizing the first COMSEC variety to generate unencrypted hostcommands. Also, the system comprises a second communication securitymodule to decrypt the encrypted hosted commands utilizing the secondCOMSEC variety to generate unencrypted hosted commands. In addition, thesystem comprises a payload on the vehicle reconfigured according to theunencrypted host commands and/or the unencrypted hosted commands.Additionally, the system comprises the payload antenna to transmitpayload data to the host receiving antenna and/or the hosted receivingantenna. Also, the system comprises the first communication securitymodule to encrypt unencrypted host telemetry utilizing the first COMSECvariety to generate encrypted host telemetry. In addition, the systemcomprises the second communication security module to encryptunencrypted hosted telemetry utilizing the second COMSEC variety togenerate encrypted hosted telemetry. Additionally, the system comprisesthe payload antenna to transmit the encrypted host telemetry to the hostreceiving antenna. Also, the system comprises the host receiving antennato transmit the encrypted host telemetry to the host SOC. In addition,the system comprises the payload antenna to transmit the encryptedhosted telemetry to the hosted receiving antenna. Further, the systemcomprises the hosted receiving antenna to transmit the encrypted hostedtelemetry to the HOC.

In at least one embodiment, a system for a virtual transponder utilizinginband commanding comprising a hosted payload (HoP) operation center(HOC) to transmit encrypted hosted commands to a hosted receivingantenna, where the encrypted hosted commands are encrypted utilizing asecond communication security (COMSEC) variety. The system furthercomprises the hosted receiving antenna to transmit the encrypted hostedcommands to a payload antenna on a vehicle. Also, the system comprises ahost spacecraft operations center (SOC) to transmit encrypted hostcommands to a host receiving antenna, where the encrypted host commandsare encrypted utilizing a first COMSEC variety. In addition, the systemcomprises the host receiving antenna to transmit the encrypted hostcommands to the payload antenna. Additionally, the system comprises afirst communication security module to decrypt the encrypted hostcommands utilizing the first COMSEC variety to generate unencrypted hostcommands. Also, the system comprises a second communication securitymodule to decrypt the encrypted hosted commands utilizing the secondCOMSEC variety to generate unencrypted hosted commands. In addition, thesystem comprises a payload on the vehicle reconfigured according to theunencrypted host commands and/or the unencrypted hosted commands.Additionally, the system comprises the payload antenna to transmitpayload data to the host receiving antenna and/or the hosted receivingantenna. Also, the system comprises the first communication securitymodule to encrypt unencrypted telemetry utilizing the first COMSECvariety to generate encrypted telemetry. In addition, the systemcomprises the payload antenna to transmit the encrypted telemetry to thehost receiving antenna. Additionally, the system comprises the hostreceiving antenna to transmit the encrypted telemetry to the host SOC.Also, the system comprises the payload antenna to transmit the encryptedtelemetry to the hosted receiving antenna. Further, the system comprisesthe hosted receiving antenna to transmit the encrypted telemetry to theHOC.

In one or more embodiments, a system for a virtual transponder utilizinginband commanding comprises a hosted payload (HoP) operation center(HOC) to transmit encrypted hosted commands to a host spacecraftoperations center (SOC). In one or more embodiments, the encryptedhosted commands are encrypted utilizing a second communication security(COMSEC) variety. The system further comprises the host SOC to transmitencrypted host commands and the encrypted hosted commands to a hostreceiving antenna. In one or more embodiments, the encrypted hostcommands are encrypted utilizing a first COMSEC variety. Also, thesystem comprises the host receiving antenna to transmit the encryptedhost commands and the encrypted hosted commands to a payload antenna onthe vehicle. In addition, the system comprises a first communicationsecurity module to decrypt the encrypted host commands utilizing thefirst COMSEC variety to generate unencrypted host commands.Additionally, the system comprises a second communication securitymodule to decrypt the encrypted hosted commands utilizing the secondCOMSEC variety to generate unencrypted hosted commands. Also, the systemcomprises a payload on the vehicle reconfigured according to at leastone of the unencrypted host commands or the unencrypted hosted commands.In addition, the system comprises the payload antenna to transmitpayload data to at least one of the host receiving antenna or a hostedreceiving antenna. Additionally, the system comprises the firstcommunication security module to encrypt unencrypted host telemetryutilizing the first COMSEC variety to generate encrypted host telemetry.In addition, the system comprises the second communication securitymodule to encrypt unencrypted hosted telemetry utilizing the secondCOMSEC variety to generate encrypted hosted telemetry. Also, the systemcomprises a host telemetry transmitter to transmit the encrypted hosttelemetry to the host SOC. In addition, the system comprises a hostedtelemetry transmitter to transmit the encrypted hosted telemetry to thehost SOC. Further, the system comprises the host SOC to transmit theencrypted hosted telemetry to the HOC.

In one or more embodiments, a method for a virtual transponder utilizinginband commanding comprises transmitting, by a hosted payload (HoP)operation center (HOC), encrypted hosted commands to a host spacecraftoperations center (SOC), where the encrypted hosted commands areencrypted utilizing a second communication security (COMSEC) variety.The method also comprises transmitting, by the host SOC, the encryptedhosted commands to a host receiving antenna. The method furthercomprises transmitting, by the host receiving antenna, the encryptedhosted commands to a payload antenna on a vehicle. Also, the methodcomprises transmitting, by the host SOC, encrypted host commands to thevehicle, where the encrypted host commands are encrypted utilizing afirst COMSEC variety. In addition, the method comprises decrypting, by afirst communication security module, the encrypted host commandsutilizing the first COMSEC variety to generate unencrypted hostcommands. Additionally, the method comprises decrypting, by a secondcommunication security module, the encrypted hosted commands utilizingthe second COMSEC variety to generate unencrypted hosted commands. Also,the method comprises reconfiguring a payload on the vehicle according tothe unencrypted host commands and/or the unencrypted hosted commands.Additionally, the method comprises transmitting, by the payload antenna,payload data to a host receiving antenna and/or the hosted receivingantenna. Also, the method comprises encrypting, by the firstcommunication security module, unencrypted host telemetry utilizing thefirst COMSEC variety to generate encrypted host telemetry. Additionally,the method comprises encrypting, by the second communication securitymodule, unencrypted hosted telemetry utilizing the second COMSEC varietyto generate encrypted hosted telemetry. In addition, the methodcomprises transmitting, by a host telemetry transmitter, the encryptedhost telemetry to the host SOC. Also, the method comprises transmitting,by a hosted telemetry transmitter, the encrypted hosted telemetry to thehost SOC. Further, the method comprises transmitting, by the host SOC,the encrypted hosted telemetry to the HOC.

In one or more embodiments, a system for a virtual transponder utilizinginband commanding comprises a hosted payload (HoP) operation center(HOC) to transmit encrypted hosted commands to a host spacecraftoperations center (SOC), where the encrypted hosted commands areencrypted utilizing a second communication security (COMSEC) variety.The system also comprises the host SOC to transmit the encrypted hostedcommands to a host receiving antenna. The system further comprises thehost receiving antenna to transmit the encrypted hosted commands to apayload antenna on a vehicle. Also, the system comprises the host SOC totransmit encrypted host commands to the vehicle, where the encryptedhost commands are encrypted utilizing a first COMSEC variety. Inaddition, the system comprises a first communication security module todecrypt the encrypted host commands utilizing the first COMSEC varietyto generate unencrypted host commands. Additionally, the systemcomprises a second communication security module to decrypt theencrypted hosted commands utilizing the second COMSEC variety togenerate unencrypted hosted commands. Also, the system comprises apayload on the vehicle reconfigured according to the unencrypted hostcommands and/or the unencrypted hosted commands. In addition, the systemcomprises the payload antenna to transmit payload data to a hostreceiving antenna and/or the hosted receiving antenna. Additionally, thesystem comprises the first communication security module to encryptunencrypted host telemetry utilizing the first COMSEC variety togenerate encrypted host telemetry. Also, the system comprises the secondcommunication security module to encrypt unencrypted hosted telemetryutilizing the second COMSEC variety to generate encrypted hostedtelemetry. In addition, the system comprises a host telemetrytransmitter to transmit the encrypted host telemetry to the host SOC.Additionally, the system comprises a hosted telemetry transmitter totransmit the encrypted hosted telemetry to the host SOC. Further, thesystem comprises the host SOC to transmit the encrypted hosted telemetryto the HOC.

In at least one embodiment, a method for a virtual transponder utilizinginband commanding comprises transmitting, by a hosted payload (HoP)operation center (HOC), encrypted hosted commands to a host spacecraftoperations center (SOC), where the encrypted hosted commands areencrypted utilizing a second communication security (COMSEC) variety.The method also comprises transmitting, by the host SOC, the encryptedhosted commands to a host receiving antenna. The method furthercomprises transmitting, by the host receiving antenna, the encryptedhosted commands to a payload antenna on a vehicle. Also, the methodcomprises transmitting, by the host SOC, encrypted host commands to ahost receiving antenna, where the encrypted host commands are encryptedutilizing a first COMSEC variety. In addition, the method comprisestransmitting, by the host receiving antenna, the encrypted host commandsto the payload antenna on the vehicle. Additionally, the methodcomprises decrypting, by a first communication security module, theencrypted host commands utilizing the first COMSEC variety to generateunencrypted host commands. Also, the method comprises decrypting, by asecond communication security module, the encrypted hosted commandsutilizing the second COMSEC variety to generate unencrypted hostedcommands. In addition, the method comprises reconfiguring a payload onthe vehicle according to the unencrypted host commands and/or theunencrypted hosted commands. Additionally, the method comprisestransmitting, by the payload antenna, payload data to the host receivingantenna and/or the hosted receiving antenna. Also, the method comprisesencrypting, by the first communication security module, unencryptedtelemetry utilizing the first COMSEC variety to generate encryptedtelemetry. In addition, the method comprises transmitting, by atelemetry transmitter, the encrypted telemetry to the host SOC. Further,the method comprises transmitting, by the host SOC, the encryptedtelemetry to the HOC.

In at least one embodiment, a system for a virtual transponder utilizinginband commanding comprises a hosted payload (HoP) operation center(HOC) to transmit encrypted hosted commands to a host spacecraftoperations center (SOC), where the encrypted hosted commands areencrypted utilizing a second communication security (COMSEC) variety.The system also comprises the host SOC to transmit the encrypted hostedcommands to a host receiving antenna. The system further comprises thehost receiving antenna to transmit the encrypted hosted commands to apayload antenna on a vehicle. Also, the system comprises the host SOC totransmit encrypted host commands to a host receiving antenna, where theencrypted host commands are encrypted utilizing a first COMSEC variety.In addition, the system comprises the host receiving antenna to transmitthe encrypted host commands to the payload antenna on the vehicle.Additionally, the system comprises a first communication security moduleto decrypt the encrypted host commands utilizing the first COMSECvariety to generate unencrypted host commands. Also, the systemcomprises a second communication security module to decrypt theencrypted hosted commands utilizing the second COMSEC variety togenerate unencrypted hosted commands. In addition, the system comprisesa payload on the vehicle reconfigured according to the unencrypted hostcommands and/or the unencrypted hosted commands. Additionally, thesystem comprises transmitting, by the payload antenna, payload data tothe host receiving antenna and/or the hosted receiving antenna. Also,the system comprises the first communication security module to encryptunencrypted telemetry utilizing the first COMSEC variety to generateencrypted telemetry. In addition, the system comprises a telemetrytransmitter to transmit the encrypted telemetry to the host SOC.Further, the system comprises the host SOC to transmit the encryptedtelemetry to the HOC.

In one or more embodiments, a method for a virtual transponder utilizinginband commanding comprises transmitting, by a hosted payload (HoP)operation center (HOC), encrypted hosted commands to a host spacecraftoperations center (SOC), where the encrypted hosted commands areencrypted utilizing a second communication security (COMSEC) variety.The method also comprises transmitting, by the host SOC, the encryptedhosted commands to a host receiving antenna. The method furthercomprises transmitting, by the host receiving antenna, the encryptedhosted commands to a payload antenna on a vehicle. Also, the methodcomprises transmitting, by the host SOC, the encrypted host commands toa host receiving antenna, where the encrypted host commands areencrypted utilizing a first COMSEC variety. In addition, the methodcomprises transmitting, by the host receiving antenna, the encryptedhost commands to the payload antenna. Additionally, the method comprisesdecrypting, by a first communication security module, the encrypted hostcommands utilizing the first COMSEC variety to generate unencrypted hostcommands. Also, the method comprises decrypting, by a secondcommunication security module, the encrypted hosted commands utilizingthe second COMSEC variety to generate unencrypted hosted commands. Inaddition, the method comprises reconfiguring a payload on the vehicleaccording to the unencrypted host commands and/or the unencrypted hostedcommands. Additionally, the method comprises transmitting, by thepayload antenna, payload data to the host receiving antenna and/or thehosted receiving antenna. Also, the method comprises encrypting, by thefirst communication security module, unencrypted host telemetryutilizing the first COMSEC variety to generate encrypted host telemetry.In addition, the method comprises encrypting, by the secondcommunication security module, unencrypted hosted telemetry utilizingthe second COMSEC variety to generate encrypted hosted telemetry.Additionally, the method comprises transmitting, by the payload antenna,the encrypted host telemetry to the host receiving antenna. Also, themethod comprises transmitting, by the host receiving antenna, theencrypted host telemetry to the host SOC. In addition, the methodcomprises transmitting, by the payload antenna, the encrypted hostedtelemetry to the host receiving antenna. Also, the method comprisestransmitting, by the host receiving antenna, the encrypted hostedtelemetry to the host SOC. Further, the method comprises the host SOC,transmitting, the encrypted hosted telemetry to the HOC.

In one or more embodiments, a system for a virtual transponder utilizinginband commanding comprises a hosted payload (HoP) operation center(HOC) to transmit encrypted hosted commands to a host spacecraftoperations center (SOC), where the encrypted hosted commands areencrypted utilizing a second communication security (COMSEC) variety.The system also comprises the host SOC to transmit the encrypted hostedcommands to a host receiving antenna. The system further comprises thehost receiving antenna to transmit the encrypted hosted commands to apayload antenna on a vehicle. Also, the system comprises a hostspacecraft operations center (SOC) to transmit the encrypted hostcommands to a host receiving antenna, where the encrypted host commandsare encrypted utilizing a first COMSEC variety. In addition, the systemcomprises the host receiving antenna to transmit the encrypted hostcommands to the payload antenna. Additionally, the system comprises afirst communication security module to decrypt the encrypted hostcommands utilizing the first COMSEC variety to generate unencrypted hostcommands. Also, the system comprises a second communication securitymodule to decrypt the encrypted hosted commands utilizing the secondCOMSEC variety to generate unencrypted hosted commands. In addition, thesystem comprises a payload on the vehicle reconfigured according to theunencrypted host commands and/or the unencrypted hosted commands.Additionally, the system comprises the payload antenna to transmitpayload data to the host receiving antenna and/or the hosted receivingantenna. Also, the system comprises the first communication securitymodule to encrypt unencrypted host telemetry utilizing the first COMSECvariety to generate encrypted host telemetry. In addition, the systemcomprises the second communication security module to encryptunencrypted hosted telemetry utilizing the second COMSEC variety togenerate encrypted hosted telemetry. Additionally, the system comprisesthe payload antenna to transmit the encrypted host telemetry to the hostreceiving antenna. Also, the system comprises the host receiving antennato transmit the encrypted host telemetry to the host SOC. In addition,the system comprises the payload antenna to transmit the encryptedhosted telemetry to the host receiving antenna. Also, the systemcomprises the host receiving antenna to transmit the encrypted hostedtelemetry to the host SOC. Further, the system comprises the host SOC totransmit the encrypted hosted telemetry to the HOC.

In at least one embodiment, a method for a virtual transponder utilizinginband commanding comprises transmitting, by a hosted payload (HoP)operation center (HOC), encrypted hosted commands to a host spacecraftoperations center (SOC), where the encrypted hosted commands areencrypted utilizing a second communication security (COMSEC) variety.The method also comprises transmitting by the host SOC the encryptedhosted commands to a host receiving antenna. The method furthercomprises transmitting, by the host receiving antenna, the encryptedhosted commands to a payload antenna on a vehicle. Also, the methodcomprises transmitting, by the host SOC, encrypted host commands to ahost receiving antenna, where the encrypted host commands are encryptedutilizing a first COMSEC variety. In addition, the method comprisestransmitting, by the host receiving antenna, the encrypted host commandsto the payload antenna. Additionally, the method comprises decrypting,by a first communication security module, the encrypted host commandsutilizing the first COMSEC variety to generate unencrypted hostcommands. Also, the method comprises decrypting, by a secondcommunication security module, the encrypted hosted commands utilizingthe second COMSEC variety to generate unencrypted hosted commands. Inaddition, the method comprises reconfiguring a payload on the vehicleaccording to the unencrypted host commands and/or the unencrypted hostedcommands. Additionally, the method comprises transmitting, by thepayload antenna, payload data to the host receiving antenna and/or thehosted receiving antenna. Also, the method comprises encrypting, by thefirst communication security module, unencrypted telemetry utilizing thefirst COMSEC variety to generate encrypted telemetry. In addition, themethod comprises transmitting, by the payload antenna, the encryptedtelemetry to the host receiving antenna. Additionally, the methodcomprises transmitting, by the host receiving antenna, the encryptedtelemetry to the host SOC. Further, the method comprises transmitting,by the host SOC, the encrypted telemetry to the HOC.

In at least one embodiment, a system for a virtual transponder utilizinginband commanding comprising a hosted payload (HoP) operation center(HOC) to transmit encrypted hosted commands to a host spacecraftoperations center (SOC), where the encrypted hosted commands areencrypted utilizing a second communication security (COMSEC) variety.The system also comprises the host SOC to transmit the encrypted hostedcommands to a host receiving antenna. The system further comprises thehost receiving antenna to transmit the encrypted hosted commands to apayload antenna on a vehicle. Also, the system comprises the host SOC totransmit encrypted host commands to a host receiving antenna, where theencrypted host commands are encrypted utilizing a first COMSEC variety.In addition, the system comprises the host receiving antenna to transmitthe encrypted host commands to the payload antenna. Additionally, thesystem comprises a first communication security module to decrypt theencrypted host commands utilizing the first COMSEC variety to generateunencrypted host commands. Also, the system comprises a secondcommunication security module to decrypt the encrypted hosted commandsutilizing the second COMSEC variety to generate unencrypted hostedcommands. In addition, the system comprises a payload on the vehiclereconfigured according to the unencrypted host commands and/or theunencrypted hosted commands. Additionally, the system comprises thepayload antenna to transmit payload data to the host receiving antennaand/or the hosted receiving antenna. Also, the system comprises thefirst communication security module to encrypt unencrypted telemetryutilizing the first COMSEC variety to generate encrypted telemetry. Inaddition, the system comprises the payload antenna to transmit theencrypted telemetry to the host receiving antenna. Additionally, thesystem comprises the host receiving antenna to transmit the encryptedtelemetry to the host SOC. Further, the system comprises the host SOC totransmit the encrypted telemetry to the HOC.

In at least one embodiment, a method for a virtual transponder on avehicle comprises generating, by a configuration algorithm (CA), aconfiguration for a portion of a payload on the vehicle utilized by ahost user by using an option for each of at least one variable for theportion of the payload on the vehicle utilized by the host user. Themethod further comprises generating, by the CA, a configuration for aportion of the payload on the vehicle utilized by a hosted user by usingan option for each of at least one variable for the portion of thepayload on the vehicle utilized by the hosted user. Also, the methodcomprises generating, by a host command generator, host commands forreconfiguring the portion of the payload on the vehicle utilized by thehost user by using the configuration for the portion of the payload onthe vehicle utilized by the host user. In addition, the method comprisesgenerating, by a hosted command generator, hosted commands forreconfiguring the portion of the payload on the vehicle utilized by thehosted user by using the configuration for the portion of the payload onthe vehicle utilized by the hosted user. Additionally, the methodcomprises transmitting the host commands and the hosted commands to thevehicle. Also, the method comprises reconfiguring the portion of thepayload on the vehicle utilized by the host user by using the hostcommands. Further the method comprises reconfiguring the portion of thepayload on the vehicle utilized by the hosted user by using the hostedcommands.

In one or more embodiments, at least one variable is: at least onetransponder power, at least one transponder spectrum, at least onetransponder gain setting, at least one transponder limiter setting, atleast one transponder automatic level control setting, at least onetransponder phase setting, at least one internal gain generation,bandwidth for at least one beam, at least one frequency band for atleast one of at least one beam, at least one transponder beamformingsetting, effective isotropic radiation power (EIRP) for at least one ofat least one beam, at least one transponder channel, and/or beamsteering for at least one of at least one beam.

In at least one embodiment, the reconfiguring comprises reconfiguring:at least one antenna, at least one analog-to-digital converter, at leastone digital-to-analog converter, at least one beamformer, at least onedigital channelizer, at least one demodulator, at least one modulator,at least one digital switch matrix, at least one digital combiner,and/or at least one analog switch matrix.

In one or more embodiments, at least one antenna a parabolic reflectorantenna, a shaped reflector antenna, a multifeed array antenna, and/or aphased array antenna.

In at least one embodiment, the host computing device and the hostedcomputing device are located at a respective station. In someembodiments, the station a ground station, a terrestrial vehicle, anairborne vehicle, or a marine vehicle.

In one or more embodiments, the vehicle is an airborne vehicle. In someembodiments, the airborne vehicle is a satellite, an aircraft, anunmanned aerial vehicle (UAV), or a space plane.

In at least one embodiment, the method further comprises selecting, witha host graphical user interface (GUI) on a host computing device, theoption for each of at least one variable for the portion of the payloadon the vehicle utilized by the host user.

In one or more embodiments, the method further comprises selecting, witha hosted GUI on a hosted computing device, the option for each of atleast one variable for the portion of the payload on the vehicleutilized by the hosted user.

In at least one embodiment, a system for a virtual transponder on avehicle comprises a configuration algorithm (CA) to generate aconfiguration for a portion of a payload on the vehicle utilized by ahost user by using an option for each of at least one variable for theportion of the payload on the vehicle utilized by the host user, and togenerate a configuration for a portion of the payload on the vehicleutilized by a hosted user by using an option for each of at least onevariable for the portion of the payload on the vehicle utilized by thehosted user. The system further comprises a host command generator togenerate host commands for reconfiguring the portion of the payload onthe vehicle utilized by the host user by using the configuration for theportion of the payload on the vehicle utilized by the host user.Further, the system comprises a hosted command generator to generatehosted commands for reconfiguring the portion of the payload on thevehicle utilized by the hosted user by using the configuration for theportion of the payload on the vehicle utilized by the hosted user. Inone or more embodiments, the portion of the payload on the vehicleutilized by the host user is reconfigured by using the host commands. Insome embodiments, the portion of the payload on the vehicle utilized bythe hosted user is reconfigured by using the hosted commands.

In one or more embodiments, the system further comprises a hostgraphical user interface (GUI), on a host computing device, used toselect the option for each of at least one variable for the portion ofthe payload on the vehicle utilized by the host user.

In at least one embodiment, the system further comprises a hosted GUI,on a hosted computing device, used to select the option for each of atleast one variable for the portion of the payload on the vehicleutilized by the hosted user.

The features, functions, and advantages can be achieved independently invarious embodiments of the present disclosure or may be combined in yetother embodiments.

DRAWINGS

These and other features, aspects, and advantages of the presentdisclosure will become better understood with regard to the followingdescription, appended claims, and accompanying drawings where:

FIG. 1 is a diagram showing simplified architecture for the disclosedsystem for a virtual transponder, in accordance with at least oneembodiment of the present disclosure.

FIGS. 2A-13H show exemplary systems and methods for a virtualtransponder utilizing inband commanding, in accordance with at least oneembodiment of the present disclosure.

FIG. 2A is a diagram showing the disclosed system for a virtualtransponder utilizing inband commanding for the hosted user using ahosted receiving antenna, in accordance with at least one embodiment ofthe present disclosure.

FIG. 2B is a diagram showing the disclosed system for a virtualtransponder utilizing inband commanding for the hosted user using a hostreceiving antenna, in accordance with at least one embodiment of thepresent disclosure.

FIGS. 3A, 3B, 3C, and 3D together show a flow chart for the disclosedmethod for a virtual transponder utilizing inband commanding for thehosted user using a hosted receiving antenna, in accordance with atleast one embodiment of the present disclosure.

FIGS. 3E, 3F, 3G, and 3H together show a flow chart for the disclosedmethod for a virtual transponder utilizing inband commanding for thehosted user using a host receiving antenna, in accordance with at leastone embodiment of the present disclosure.

FIG. 4 is a diagram showing the disclosed system for a virtualtransponder utilizing inband commanding for the host user, in accordancewith at least one embodiment of the present disclosure.

FIGS. 5A, 5B, 5C, and 5D together show a flow chart for the disclosedmethod for a virtual transponder utilizing inband commanding for thehost user, in accordance with at least one embodiment of the presentdisclosure.

FIG. 6A is a diagram showing the disclosed system for a virtualtransponder utilizing inband commanding for the host user and the hosteduser using two receiving antennas and employing two communicationsecurity (COMSEC) varieties for telemetry, in accordance with at leastone embodiment of the present disclosure.

FIG. 6B is a diagram showing the disclosed system for a virtualtransponder utilizing inband commanding for the host user and the hosteduser using one receiving antenna and employing two communicationsecurity (COMSEC) varieties for telemetry, in accordance with at leastone embodiment of the present disclosure.

FIGS. 7A, 7B, 7C, and 7D together show a flow chart for the disclosedmethod for a virtual transponder utilizing inband commanding for thehost user and the hosted user using two receiving antennas and employingtwo COMSEC varieties for telemetry, in accordance with at least oneembodiment of the present disclosure.

FIGS. 7E, 7F, 7G, and 7H together show a flow chart for the disclosedmethod for a virtual transponder utilizing inband commanding for thehost user and the hosted user using one receiving antenna and employingtwo communication security (COMSEC) varieties for telemetry, inaccordance with at least one embodiment of the present disclosure.

FIG. 8A is a diagram showing the disclosed system for a virtualtransponder utilizing inband commanding for the host user and the hosteduser using two receiving antennas and employing one COMSEC variety fortelemetry, in accordance with at least one embodiment of the presentdisclosure.

FIG. 8B is a diagram showing the disclosed system for a virtualtransponder utilizing inband commanding for the host user and the hosteduser using one receiving antenna and employing one COMSEC variety fortelemetry, in accordance with at least one embodiment of the presentdisclosure.

FIGS. 9A, 9B, 9C, and 9D together show a flow chart for the disclosedmethod for a virtual transponder utilizing inband commanding for thehost user and the hosted user using two receiving antennas and employingone COMSEC variety for telemetry, in accordance with at least oneembodiment of the present disclosure.

FIGS. 9E, 9F, 9G, and 9H together show a flow chart for the disclosedmethod for a virtual transponder utilizing inband commanding for thehost user and the hosted user using one receiving antenna and employingone COMSEC variety for telemetry, in accordance with at least oneembodiment of the present disclosure.

FIG. 10A is a diagram showing the disclosed system for a virtualtransponder utilizing inband telemetry and commanding for the host userand the hosted user using two receiving antennas and employing twoCOMSEC varieties for telemetry, in accordance with at least oneembodiment of the present disclosure.

FIG. 10B is a diagram showing the disclosed system for a virtualtransponder utilizing inband telemetry and commanding for the host userand the hosted user using one receiving antenna and employing two COMSECvarieties for telemetry, in accordance with at least one embodiment ofthe present disclosure.

FIGS. 11A, 11B, 11C, and 11D together show a flow chart for thedisclosed method for a virtual transponder utilizing inband telemetryand commanding for the host user and the hosted user using two receivingantennas and employing two COMSEC varieties for telemetry, in accordancewith at least one embodiment of the present disclosure.

FIGS. 11E, 11F, 11G, and 11H together show a flow chart for thedisclosed method for a virtual transponder utilizing inband telemetryand commanding for the host user and the hosted user using one receivingantenna and employing two COMSEC varieties for telemetry, in accordancewith at least one embodiment of the present disclosure.

FIG. 12A is a diagram showing the disclosed system for a virtualtransponder utilizing inband telemetry and commanding for the host userand the hosted user using two receiving antennas and employing oneCOMSEC variety for telemetry, in accordance with at least one embodimentof the present disclosure.

FIG. 12B is a diagram showing the disclosed system for a virtualtransponder utilizing inband telemetry and commanding for the host userand the hosted user using one receiving antenna and employing one COMSECvariety for telemetry, in accordance with at least one embodiment of thepresent disclosure.

FIGS. 13A, 13B, 13C, and 13D together show a flow chart for thedisclosed method for a virtual transponder utilizing inband telemetryand commanding for the host user and the hosted user using two receivingantennas and employing one COMSEC variety for telemetry, in accordancewith at least one embodiment of the present disclosure.

FIGS. 13E, 13F, 13G, and 13H together show a flow chart for thedisclosed method for a virtual transponder utilizing inband telemetryand commanding for the host user and the hosted user using one receivingantenna and employing one COMSEC variety for telemetry, in accordancewith at least one embodiment of the present disclosure.

FIGS. 14-19B show exemplary systems and methods for a virtualtransponder, in accordance with at least one embodiment of the presentdisclosure.

FIG. 14 is a diagram showing the disclosed system for a virtualtransponder on a vehicle, in accordance with at least one embodiment ofthe present disclosure.

FIG. 15 is a diagram showing an exemplary allocation of bandwidthamongst a plurality of beams when utilizing the disclosed virtualtransponder, in accordance with at least one embodiment of the presentdisclosure.

FIG. 16 is a diagram showing the switch architecture for a flexibleallocation of bandwidth amongst a plurality of beams when utilizing thedisclosed virtual transponder, in accordance with at least oneembodiment of the present disclosure.

FIG. 17 is a diagram showing details of the digital channelizer of FIG.16, in accordance with at least one embodiment of the presentdisclosure.

FIG. 18 is a diagram showing exemplary components on the vehicle thatmay be utilized by the disclosed virtual transponder, in accordance withat least one embodiment of the present disclosure.

FIGS. 19A and 19B together show a flow chart for the disclosed methodfor a virtual transponder on a vehicle, in accordance with at least oneembodiment of the present disclosure.

DESCRIPTION

The methods and apparatus disclosed herein provide an operative systemfor virtual transponders utilizing inband commanding. The system of thepresent disclosure allows for vehicle operators to privately sharevehicle resources. It should be noted that in this disclosure, in-bandfrequency band(s) refer to a frequency band(s) that is the samefrequency band(s) utilized to transmit payload data; and out-of-bandfrequency band(s) refer to a frequency band(s) that is not the samefrequency band(s) utilized to transmit payload data.

As previously mentioned above, currently, typical transponders on avehicle (e.g., a satellite) have the ability to perform switching ofinputs to outputs of the payload. All of this switching on the payloadis commanded and controlled by a single satellite controller with noresource allocation privacy. For example, in a digital transponder, whena user request for a channel with specific bandwidth and antennacharacteristics is made, the channel is then set up, used, and thendisconnected.

The disclosed system allows for private vehicle resource allocation andcontrol that provides vehicle users the ability to privately,dynamically, allocate resources on demand. In particular, the disclosedsystem employs a virtual transponder, which is a transponder partitionedinto multiple transponders with independent command and control. In oneor more embodiments, an exemplary virtual transponder includes a digitaltransponder with a digital channelizer, a digital switch matrix, and adigital combiner that is configured to partition a digital transponderinto multiple transponders with independent command and control. Commandand control of the virtual transponder is achieved via ground softwarethat provides dynamic allocation and privatization of the digital switchmatrix for bandwidth on demand.

It should be noted that the disclosed system for private vehicleresource allocation and control may employ various different types oftransponders for the virtual transponder other than the specificdisclosed embodiments (e.g., depicted FIGS. 16-18) for the virtualtransponder. For example, various different types of transponders may beemployed for the virtual transponder including, but not limited to,various different types of digital transponders, various different typesof analog transponders (e.g., conventional repeater-type transponders),and various different types of combination analog/digital transponders.

In the following description, numerous details are set forth in order toprovide a more thorough description of the system. It will be apparent,however, to one skilled in the art, that the disclosed system may bepracticed without these specific details. In the other instances, wellknown features have not been described in detail so as not tounnecessarily obscure the system.

Embodiments of the present disclosure may be described herein in termsof functional and/or logical components and various processing steps. Itshould be appreciated that such components may be realized by any numberof hardware, software, and/or firmware components configured to performthe specified functions. For example, an embodiment of the presentdisclosure may employ various integrated circuit components (e.g.,memory elements, digital signal processing elements, logic elements,look-up tables, or the like), which may carry out a variety of functionsunder the control of one or more processors, microprocessors, or othercontrol devices. In addition, those skilled in the art will appreciatethat embodiments of the present disclosure may be practiced inconjunction with other components, and that the system described hereinis merely one example embodiment of the present disclosure.

For the sake of brevity, conventional techniques and components relatedto satellite communication systems, and other functional aspects of thesystem (and the individual operating components of the systems) may notbe described in detail herein. Furthermore, the connecting lines shownin the various figures contained herein are intended to representexample functional relationships and/or physical couplings between thevarious elements. It should be noted that many alternative or additionalfunctional relationships or physical connections may be present in anembodiment of the present disclosure.

FIG. 1 is a diagram 100 showing simplified architecture for thedisclosed system for a virtual transponder, in accordance with at leastone embodiment of the present disclosure. In this figure, a simplifiedview of multiple possible hosted payload configurations is illustrated.In particular, this figure shows a space segment 110 and a groundsegment 120. The space segment 110 represents a vehicle. Variousdifferent types of vehicles may be employed for the vehicle including,but not limited to, an airborne vehicle. And, various different types ofairborne vehicles may be employed for the vehicle including, but notlimited to, a satellite, an aircraft, an unmanned aerial vehicle (UAV),and a space plane.

In the case of a satellite being employed for the vehicle, it should benoted that satellites typically include computer-controlled systems. Asatellite generally includes a bus 130 and a payload 140. The bus 130may include systems (which include components) that control thesatellite. These systems perform tasks, such as power generation andcontrol, thermal control, telemetry, attitude control, orbit control,and other suitable operations.

The payload 140 of the satellite provides functions to users of thesatellite. The payload 140 may include antennas, transponders, and othersuitable devices. For example, with respect to communications, thepayload 140 in a satellite may be used to provide Internet access,telephone communications, radio, television, and other types ofcommunications.

The payload 140 of the satellite may be used by different entities. Forexample, the payload 140 may be used by the owner of the satellite (i.e.the host user), one or more customers (i.e. the hosted user(s)), or somecombination thereof.

For example, the owner of a satellite may lease different portions ofthe payload 140 to different customers. In one example, one group ofantenna beams generated by the payload 140 of the satellite may beleased to one customer, while a second group of antenna beams may beleased to a second customer. In another example, one group of antennabeams generated by the payload 140 of the satellite may be utilized bythe owner of the satellite, while a second group of antenna beams may beleased to a customer. In yet another example, some or all of the antennabeams generated by the payload 140 of the satellite may be shared by onecustomer and a second customer. In another example, some or all of theantenna beams generated by the payload 140 of the satellite may beshared by the owner of the satellite and a customer. When satellites areshared by different users, users may have a shared communications link(e.g., Interface A) to the satellite, or each user may have a separatecommunications link (e.g., Interfaces A and D) to the satellite.

Leasing a satellite to multiple customers may increase the revenues thatan owner of a satellite can obtain. Further, a customer may use a subsetof the total resources in a satellite for a cost that is less than thecost for the customer to purchase and operate a satellite, to build andoperate a satellite, or to lease an entire satellite.

Referring back to FIG. 1, the ground segment 120 comprises a hostspacecraft operations center (SOC) (e.g., a ground station associatedwith the owner of the satellite) 150, and a hosted payload (HoP)operation center(s) (HOC(s)) (e.g., a ground station(s) associated witha customer(s) that is leasing at least a portion of the payload of thesatellite from the owner) 160.

FIG. 1 shows a number of different possible communication links (i.e.Interfaces A-E). It should be noted that the disclosed system may employsome or all of these illustrated communication links. Interface A, whichmay comprise multiple links, is an out-of-band command and telemetrylink from the host SOC 150 to command the satellite. Interface B, whichmay comprise multiple links, is a communication link, between the bus130 and the payload 140. Interface B may be used to control essentialitems, such as power. Information that may be communicated from the bus130 to the payload 140 via Interface B may include, but is not limitedto, time, ephemeris, and payload commands. Information that may becommunicated from the payload 140 to the bus 130 via Interface B mayinclude, but is not limited to, payload telemetry.

Interface C, which may comprise multiple links, is an inband command andtelemetry link for bus and/or payload. Interface D, which may comprisemultiple links, is a command and telemetry link from the HOC(s) 160 tocommand the satellite. Interface E, which may comprise multiple links,between the host SOC 150 and the HOCs 160 allows for requests from theHOCs for resource sharing of the payload 140.

FIGS. 2A-13H show exemplary systems and methods for a virtualtransponder utilizing inband commanding, in accordance with at least oneembodiment of the present disclosure.

FIG. 2A is a diagram 200 showing the disclosed system for a virtualtransponder utilizing inband commanding for the hosted user (i.e. HOC)260 using a hosted receiving antenna 290, in accordance with at leastone embodiment of the present disclosure. In this figure, a vehicle 210,a host SOC 250, and a HOC 260 are shown. The HOC 260 has leased at leasta portion (e.g., a virtual transponder(s)) of the payload 205 of thevehicle 210 from the owner of a satellite (i.e. the host SOC) 250. Itshould be noted that in some embodiments, the HOC 260 may lease all ofthe payload 205 of the vehicle 210 from the owner of a satellite (i.e.the host SOC) 250. Also, it should be noted that is some embodiments,the HOC 260 may own the payload 205 (e.g., a steerable antenna) of thevehicle 210, and contract the host SOC 250 to transmit encrypted hostedcommands to the vehicle 210.

During operation, the HOC 260 encrypts unencrypted hosted commands (i.e.unencrypted HoP CMD), by utilizing a second COMSEC variety, to produceencrypted hosted commands (i.e. encrypted HoP CMD). The hosted commandsare commands that are used to configure the portion (e.g., a virtualtransponder(s)) of the payload 205 that the HOC 260 is leasing from thehost SOC 250. The host SOC 250 encrypts unencrypted host commands (i.e.unencrypted host CMD), by utilizing a first COMSEC variety, to produceencrypted host commands (i.e. encrypted host CMD). The host commands arecommands that are used to configure the portion (e.g., a transponder(s))of the payload 205 that host SOC 250 is utilizing for itself.

It should be noted that, although in FIG. 2A the host SOC 250 isdepicted to have its ground antenna located right next to its operationsbuilding; in other embodiments, the host SOC 250 may have its groundantenna located very far away from the its operations building (e.g.,the ground antenna may be located in another country than the operationsbuilding).

Also, it should be noted that the first COMSEC variety may include atleast one encryption key and/or at least one algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm). Additionally, itshould be noted that the second COMSEC variety may include at least oneencryption key and/or at least one encryption algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm).

The HOC 260 then transmits 215 the encrypted hosted commands to a hostedreceiving antenna 290. After the hosted receiving antenna 290 receivesthe encrypted hosted commands, the hosted receiving antenna 290transmits 297 the encrypted hosted commands to a payload antenna 280 onthe vehicle 210. The hosted receiving antenna 290 transmits 297 theencrypted hosted commands utilizing an in-band frequency band(s) (i.e. afrequency band(s) that is the same frequency band(s) utilized totransmit payload data). The payload antenna 280 transmits the encryptedhosted commands to a payload 205. The payload 205 on the vehicle 210receives the encrypted hosted commands. The payload 205 then transmits255 the encrypted hosted commands to a second communication securitymodule 265. The second communication security module 265 decrypts theencrypted hosted commands utilizing the second COMSEC variety (i.e.COMSEC Variety 2) to generate unencrypted hosted commands.

It should be noted that the second communication security module 265 maycomprise one or more modules. In addition, the second communicationsecurity module 265 may comprise one or more processors.

The host SOC 250 transmits 220 the encrypted host commands to thevehicle 210. The host SOC 250 transmits 220 the encrypted host commandsutilizing an out-of-band frequency band(s) (i.e. a frequency band(s)that is not the same frequency band(s) utilized to transmit payloaddata). The host command receiver 235 on the vehicle 210 receives theencrypted host commands.

The host command receiver 235 then transmits 252 the encrypted hostcommands to a first communication security module 262. The firstcommunication security module 262 decrypts the encrypted host commandsutilizing the first COMSEC variety (i.e. COMSEC Variety 1) to generateunencrypted host commands.

It should be noted that the first communication security module 262 maycomprise one or more modules. In addition, the first communicationsecurity module 262 may comprise one or more processors.

The first communication security module 262 then transmits 270 theunencrypted host commands to the payload (i.e. the shared host/hostedpayload) 205. The second communication security module 265 transmits 275the unencrypted hosted commands to the payload (i.e. the sharedhost/hosted payload) 205. The payload 205 is reconfigured according tothe unencrypted host commands and/or the unencrypted hosted commands.The payload antenna 280 then transmits (e.g., in one or more antennabeams 281) payload data to a host receiving antenna 285 and/or thehosted receiving antenna 290 on the ground.

Also, it should be noted that, although in FIG. 2A, antenna beams 281 isshown to include a plurality of circular spot beams; in otherembodiments, antenna beams 281 may include more or less number of beamsthan is shown in FIG. 2A (e.g., antenna beams 281 may only include asingle beam), and antenna beams 281 may include beams of differentshapes than circular spot beams as is shown in FIG. 2A (e.g., antennabeams 281 may include elliptical beams and/or shaped beams of variousdifferent shapes).

It should be noted that in one or more embodiments, the payload antenna280 may comprise one or more reflector dishes including, but not limitedto, parabolic reflectors and/or shaped reflectors. In some embodiments,the payload antenna 280 may comprise one or more multifeed antennaarrays.

The payload 205 transmits 291 unencrypted host telemetry (i.e.unencrypted host TLM, which is telemetry data related to the portion ofthe payload 205 that is utilized by the host SOC 250) to the firstcommunication security module 262. The first communication securitymodule 262 then encrypts the unencrypted host telemetry utilizing thefirst COMSEC variety to generate encrypted host telemetry (i.e.encrypted host TLM).

The payload 205 transmits 292 unencrypted hosted telemetry (i.e.unencrypted HoP TLM, which is telemetry data related to the portion ofthe payload 205 that is leased by the HOC 260) to the secondcommunication security module 265. The second communication securitymodule 265 then encrypts the unencrypted hosted telemetry utilizing thesecond COMSEC variety to generate encrypted hosted telemetry (i.e.encrypted HoP TLM).

The first communication security module 262 then transmits 293 theencrypted host telemetry to a host telemetry transmitter 289. The hosttelemetry transmitter 289 then transmits 295 the encrypted hosttelemetry to the host SOC 250. The host telemetry transmitter 289transmits 295 the encrypted host telemetry utilizing an out-of-bandfrequency band(s). The host SOC 250 then decrypts the encrypted hosttelemetry utilizing the first COMSEC variety to generate the unencryptedhost telemetry.

The second communication security module 265 then transmits 296 theencrypted hosted telemetry to a hosted telemetry transmitter 294. Thehosted telemetry transmitter 294 then transmits 298 the encrypted hostedtelemetry to the host SOC 250. The telemetry transmitter 294 transmits298 the encrypted hosted telemetry utilizing an out-of-band frequencyband(s). The host SOC 250 then transmits 299 the encrypted hostedtelemetry to the HOC 260. The HOC 260 then decrypts the encrypted hostedtelemetry utilizing the second COMSEC variety to generate theunencrypted hosted telemetry.

FIG. 2B is a diagram 2000 showing the disclosed system for a virtualtransponder utilizing inband commanding for the hosted user (i.e. HOC)2060 using a host receiving antenna 20085, in accordance with at leastone embodiment of the present disclosure. In this figure, a vehicle2010, a host SOC 2050, and a HOC 2060 are shown. The HOC 2060 has leasedat least a portion (e.g., a virtual transponder(s)) of the payload 2005of the vehicle 2010 from the owner of a satellite (i.e. the host SOC)2050. It should be noted that in some embodiments, the HOC 2060 maylease all of the payload 2005 of the vehicle 2010 from the owner of asatellite (i.e. the host SOC) 2050. Also, it should be noted that issome embodiments, the HOC 2060 may own the payload 2005 (e.g., asteerable antenna) of the vehicle 2010, and contract the host SOC 2050to transmit encrypted hosted commands to the vehicle 2010.

During operation, the HOC 2060 encrypts unencrypted hosted commands(i.e. unencrypted HoP CMD), by utilizing a second COMSEC variety, toproduce encrypted hosted commands (i.e. encrypted HoP CMD). The hostedcommands are commands that are used to configure the portion (e.g., avirtual transponder(s)) of the payload 2005 that the HOC 2060 is leasingfrom the host SOC 2050. The host SOC 2050 encrypts unencrypted hostcommands (i.e. unencrypted host CMD), by utilizing a first COMSECvariety, to produce encrypted host commands (i.e. encrypted host CMD).The host commands are commands that are used to configure the portion(e.g., a transponder(s)) of the payload 2005 that host SOC 2050 isutilizing for itself.

It should be noted that, although in FIG. 2B the host SOC 2050 isdepicted to have its ground antenna located right next to its operationsbuilding; in other embodiments, the host SOC 2050 may have its groundantenna located very far away from the its operations building (e.g.,the ground antenna may be located in another country than the operationsbuilding).

Also, it should be noted that the first COMSEC variety may include atleast one encryption key and/or at least one algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm). Additionally, itshould be noted that the second COMSEC variety may include at least oneencryption key and/or at least one encryption algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm).

The HOC 2060 then transmits 2015 the encrypted hosted commands to thehost SOC 2050. Then, the host SOC 2050 transmits 2016 the encryptedhosted commands to a host receiving antenna 2085. After the hostreceiving antenna 2085 receives the encrypted hosted commands, the hostreceiving antenna 2085 transmits 2097 the encrypted hosted commands to apayload antenna 2080 on the vehicle 2010. The host receiving antenna2085 transmits 2097 the encrypted hosted commands utilizing an in-bandfrequency band(s) (i.e. a frequency band(s) that is the same frequencyband(s) utilized to transmit payload data). The payload antenna 2080transmits the encrypted hosted commands to a payload 2005. The payload2005 on the vehicle 2010 receives the encrypted hosted commands. Thepayload 2005 then transmits 2055 the encrypted hosted commands to asecond communication security module 2065. The second communicationsecurity module 2065 decrypts the encrypted hosted commands utilizingthe second COMSEC variety (i.e. COMSEC Variety 2) to generateunencrypted hosted commands.

It should be noted that the second communication security module 2065may comprise one or more modules. In addition, the second communicationsecurity module 2065 may comprise one or more processors.

The host SOC 2050 transmits 2020 the encrypted host commands to thevehicle 2010. The host SOC 2050 transmits 2020 the encrypted hostcommands utilizing an out-of-band frequency band(s) (i.e. a frequencyband(s) that is not the same frequency band(s) utilized to transmitpayload data). The host command receiver 2035 on the vehicle 2010receives the encrypted host commands.

The host command receiver 2035 then transmits 2052 the encrypted hostcommands to a first communication security module 2062. The firstcommunication security module 2062 decrypts the encrypted host commandsutilizing the first COMSEC variety (i.e. COMSEC Variety 1) to generateunencrypted host commands.

It should be noted that the first communication security module 2062 maycomprise one or more modules. In addition, the first communicationsecurity module 2062 may comprise one or more processors.

The first communication security module 2062 then transmits 2070 theunencrypted host commands to the payload (i.e. the shared host/hostedpayload) 2005. The second communication security module 2065 transmits2075 the unencrypted hosted commands to the payload (i.e. the sharedhost/hosted payload) 2005. The payload 2005 is reconfigured according tothe unencrypted host commands and/or the unencrypted hosted commands.The payload antenna 2080 then transmits (e.g., in one or more antennabeams 2081) payload data to a host receiving antenna 2085 and/or thehosted receiving antenna 2090 on the ground.

Also, it should be noted that, although in FIG. 2B, antenna beams 2081is shown to include a plurality of circular spot beams; in otherembodiments, antenna beams 2081 may include more or less number of beamsthan is shown in FIG. 2B (e.g., antenna beams 2081 may only include asingle beam), and antenna beams 2081 may include beams of differentshapes than circular spot beams as is shown in FIG. 2B (e.g., antennabeams 2081 may include elliptical beams and/or shaped beams of variousdifferent shapes).

It should be noted that in one or more embodiments, the payload antenna2080 may comprise one or more reflector dishes including, but notlimited to, parabolic reflectors and/or shaped reflectors. In someembodiments, the payload antenna 2080 may comprise one or more multifeedantenna arrays.

The payload 2005 transmits 2091 unencrypted host telemetry (i.e.unencrypted host TLM, which is telemetry data related to the portion ofthe payload 2005 that is utilized by the host SOC 2050) to the firstcommunication security module 2062. The first communication securitymodule 2062 then encrypts the unencrypted host telemetry utilizing thefirst COMSEC variety to generate encrypted host telemetry (i.e.encrypted host TLM).

The payload 2005 transmits 2092 unencrypted hosted telemetry (i.e.unencrypted HoP TLM, which is telemetry data related to the portion ofthe payload 2005 that is leased by the HOC 2060) to the secondcommunication security module 2065. The second communication securitymodule 2065 then encrypts the unencrypted hosted telemetry utilizing thesecond COMSEC variety to generate encrypted hosted telemetry (i.e.encrypted HoP TLM).

The first communication security module 2062 then transmits 2093 theencrypted host telemetry to a host telemetry transmitter 2089. The hosttelemetry transmitter 2089 then transmits 2095 the encrypted hosttelemetry to the host SOC 2050. The host telemetry transmitter 2089transmits 2095 the encrypted host telemetry utilizing an out-of-bandfrequency band(s). The host SOC 2050 then decrypts the encrypted hosttelemetry utilizing the first COMSEC variety to generate the unencryptedhost telemetry.

The second communication security module 2065 then transmits 2096 theencrypted hosted telemetry to a hosted telemetry transmitter 2094. Thehosted telemetry transmitter 2094 then transmits 2098 the encryptedhosted telemetry to the host SOC 2050. The telemetry transmitter 2094transmits 2098 the encrypted hosted telemetry utilizing an out-of-bandfrequency band(s). The host SOC 2050 then transmits 2099 the encryptedhosted telemetry to the HOC 2060. The HOC 2060 then decrypts theencrypted hosted telemetry utilizing the second COMSEC variety togenerate the unencrypted hosted telemetry.

FIGS. 3A, 3B, 3C, and 3D together show a flow chart for the disclosedmethod for a virtual transponder utilizing inband commanding for thehosted user using a hosted receiving antenna, in accordance with atleast one embodiment of the present disclosure. At the start 300 of themethod, a hosted payload (HoP) operation center (HOC) encryptsunencrypted hosted commands by utilizing a second communication security(COMSEC) variety to produce encrypted hosted commands 305. Then, the HOCtransmits the encrypted hosted commands to a hosted receiving antenna310. The hosted receiving antenna then transmits the encrypted hostedcommands to a payload antenna on a vehicle 315. Then, the payloadantenna transmits the encrypted hosted commands to a payload 320. Thepayload then transmits the encrypted hosted commands to a secondcommunication security module 325.

Then, a host spacecraft operations center (SOC) encrypts unencryptedhost commands by utilizing a first COMSEC variety to produce encryptedhost commands 330. The host SOC then transmits the encrypted hostcommands to the vehicle 335. Then, a host command receiver on thevehicle receives the encrypted host commands 340. The host commandreceiver then transmits the encrypted host commands to a firstcommunication security module 345. Then, the first communicationsecurity module decrypts the encrypted host commands utilizing the firstCOMSEC variety to generate the unencrypted host commands 350. The secondcommunication security module decrypts the encrypted hosted commandsutilizing the second COMSEC variety to generate the unencrypted hostedcommands 355. Then, the first communication security module transmitsthe unencrypted host commands to the payload 360. The secondcommunication security module transmits the unencrypted hosted commandsto the payload 365.

Then, the payload is reconfigured according to the unencrypted hostcommands and/or the unencrypted hosted commands 370. The payload antennathen transmits payload data to a host receiving antenna and/or thehosted receiving antenna 375. Then, the payload transmits to the firstcommunication security module unencrypted host telemetry 380. Thepayload transmits to the second communication security moduleunencrypted hosted telemetry 385. Then, the first communication securitymodule encrypts the unencrypted host telemetry utilizing the firstCOMSEC variety to generate encrypted host telemetry 390. The secondcommunication security module encrypts the unencrypted hosted telemetryutilizing the second COMSEC variety to generate encrypted hostedtelemetry 391.

Then, the first communication security module transmits the encryptedhost telemetry to a host telemetry transmitter 392. The host telemetrytransmitter then transmits the encrypted host telemetry to the host SOC393. Then, the host SOC decrypts the encrypted host telemetry utilizingthe first COMSEC variety to generate the unencrypted host telemetry 394.

Then, the second communication security module transmits the encryptedhosted telemetry to a hosted telemetry transmitter 395. The hostedtelemetry transmitter then transmits the encrypted hosted telemetry tothe host SOC 396. Then, the host SOC transmits the encrypted hostedtelemetry to the HOC 397. The HOC then decrypts the encrypted hostedtelemetry utilizing the second COMSEC variety to generate theunencrypted hosted telemetry 398. Then, the method ends 399.

FIGS. 3E, 3F, 3G, and 3H together show a flow chart for the disclosedmethod for a virtual transponder utilizing inband commanding for thehosted user using a host receiving antenna, in accordance with at leastone embodiment of the present disclosure. At the start 3000 of themethod, a hosted payload (HoP) operation center (HOC) encryptsunencrypted hosted commands by utilizing a second communication security(COMSEC) variety to produce encrypted hosted commands 3005. Then, theHOC transmits the encrypted hosted commands to a host spacecraftoperations center (SOC) 3010. The host SOC then transmits the encryptedhosted commands to a host receiving antenna 3012. The host receivingantenna then transmits the encrypted hosted commands to a payloadantenna on a vehicle 3015. Then, the payload antenna transmits theencrypted hosted commands to a payload 3020. The payload then transmitsthe encrypted hosted commands to a second communication security module3025.

Then, a host SOC encrypts unencrypted host commands by utilizing a firstCOMSEC variety to produce encrypted host commands 3030. The host SOCthen transmits the encrypted host commands to the vehicle 3035. Then, ahost command receiver on the vehicle receives the encrypted hostcommands 3040. The host command receiver then transmits the encryptedhost commands to a first communication security module 3045. Then, thefirst communication security module decrypts the encrypted host commandsutilizing the first COMSEC variety to generate the unencrypted hostcommands 3050. The second communication security module decrypts theencrypted hosted commands utilizing the second COMSEC variety togenerate the unencrypted hosted commands 3055. Then, the firstcommunication security module transmits the unencrypted host commands tothe payload 3060. The second communication security module transmits theunencrypted hosted commands to the payload 3065.

Then, the payload is reconfigured according to the unencrypted hostcommands and/or the unencrypted hosted commands 3070. The payloadantenna then transmits payload data to a host receiving antenna and/orthe hosted receiving antenna 3075. Then, the payload transmits to thefirst communication security module unencrypted host telemetry 3080. Thepayload transmits to the second communication security moduleunencrypted hosted telemetry 3085. Then, the first communicationsecurity module encrypts the unencrypted host telemetry utilizing thefirst COMSEC variety to generate encrypted host telemetry 3090. Thesecond communication security module encrypts the unencrypted hostedtelemetry utilizing the second COMSEC variety to generate encryptedhosted telemetry 3091.

Then, the first communication security module transmits the encryptedhost telemetry to a host telemetry transmitter 3092. The host telemetrytransmitter then transmits the encrypted host telemetry to the host SOC3093. Then, the host SOC decrypts the encrypted host telemetry utilizingthe first COMSEC variety to generate the unencrypted host telemetry3094.

Then, the second communication security module transmits the encryptedhosted telemetry to a hosted telemetry transmitter 3095. The hostedtelemetry transmitter then transmits the encrypted hosted telemetry tothe host SOC 3096. Then, the host SOC transmits the encrypted hostedtelemetry to the HOC 3097. The HOC then decrypts the encrypted hostedtelemetry utilizing the second COMSEC variety to generate theunencrypted hosted telemetry 3098. Then, the method ends 3099.

FIG. 4 is a diagram 400 showing the disclosed system for a virtualtransponder utilizing inband commanding for the host user (i.e. hostSOC) 450, in accordance with at least one embodiment of the presentdisclosure. In this figure, a vehicle 410, a host SOC 450, and a HOC 460are shown. The HOC 460 has leased at least a portion (e.g., a virtualtransponder(s)) of the payload 405 of the vehicle 410 from the owner ofa satellite (i.e. the host SOC) 450. It should be noted that in someembodiments, the HOC 460 may lease all of the payload 405 of the vehicle410 from the owner of a satellite (i.e. the host SOC) 450. Also, itshould be noted that is some embodiments, the HOC 460 may own thepayload 405 (e.g., a steerable antenna) of the vehicle 410, and contractthe host SOC 450 to transmit encrypted hosted commands to the vehicle410.

During operation, the HOC 460 encrypts unencrypted hosted commands (i.e.unencrypted HoP CMD), by utilizing a second COMSEC variety, to produceencrypted hosted commands (i.e. encrypted HoP CMD). The hosted commandsare commands that are used to configure the portion (e.g., a virtualtransponder(s)) of the payload 405 that the HOC 460 is leasing from thehost SOC 450. The host SOC 450 encrypts unencrypted host commands (i.e.unencrypted host CMD), by utilizing a first COMSEC variety, to produceencrypted host commands (i.e. encrypted host CMD). The host commands arecommands that are used to configure the portion (e.g., a transponder(s))of the payload 405 that host SOC 450 is utilizing for itself.

It should be noted that, although in FIG. 4 the host SOC 450 is depictedto have its ground antenna located right next to its operationsbuilding; in other embodiments, the host SOC 450 may have its groundantenna located very far away from the its operations building (e.g.,the ground antenna may be located in another country than the operationsbuilding).

Also, it should be noted that the first COMSEC variety may include atleast one encryption key and/or at least one algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm). Additionally, itshould be noted that the second COMSEC variety may include at least oneencryption key and/or at least one encryption algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm).

The host SOC 450 then transmits 420 the encrypted host commands to ahost receiving antenna 485. After the host receiving antenna 485receives the encrypted host commands, the host receiving antenna 485transmits 497 the encrypted host commands to a payload antenna 480 onthe vehicle 410. The host receiving antenna 485 transmits 497 theencrypted host commands utilizing an in-band frequency band(s) (i.e. afrequency band(s) that is the same frequency band(s) utilized totransmit payload data). The payload antenna 480 transmits the encryptedhost commands to a payload 405. The payload 405 on the vehicle 410receives the encrypted host commands. The payload 405 then transmits 452the encrypted host commands to a first communication security module462. The first communication security module 462 decrypts the encryptedhost commands utilizing the first COMSEC variety (i.e. COMSEC Variety 1)to generate unencrypted host commands.

It should be noted that the first communication security module 462 maycomprise one or more modules. In addition, the first communicationsecurity module 462 may comprise one or more processors.

The HOC 460 transmits 415 the encrypted hosted commands to the host SOC450. The host SOC 450 transmits 425 the encrypted hosted commands to thevehicle 410. The host SOC 450 transmits 425 the encrypted hostedcommands utilizing an out-of-band frequency band(s) (i.e. a frequencyband(s) that is not the same frequency band(s) utilized to transmitpayload data). The hosted command receiver 435 on the vehicle 410receives the encrypted host commands.

The hosted command receiver 435 then transmits 455 the encrypted hostedcommands to a second communication security module 465. The secondcommunication security module 465 decrypts the encrypted hosted commandsutilizing the second COMSEC variety (i.e. COMSEC Variety 2) to generateunencrypted hosted commands.

It should be noted that the second communication security module 465 maycomprise one or more modules. In addition, the second communicationsecurity module 465 may comprise one or more processors.

The first communication security module 462 then transmits 470 theunencrypted host commands to the payload (i.e. the shared host/hostedpayload) 405. The second communication security module 465 transmits 475the unencrypted hosted commands to the payload (i.e. the sharedhost/hosted payload) 405. The payload 405 is reconfigured according tothe unencrypted host commands and/or the unencrypted hosted commands.The payload antenna 480 then transmits (e.g., in one or more antennabeams 481) payload data to a host receiving antenna 485 and/or thehosted receiving antenna 490 on the ground.

Also, it should be noted that, although in FIG. 4, antenna beams 481 isshown to include a plurality of circular spot beams; in otherembodiments, antenna beams 481 may include more or less number of beamsthan is shown in FIG. 4 (e.g., antenna beams 481 may only include asingle beam), and antenna beams 481 may include beams of differentshapes than circular spot beams as is shown in FIG. 4 (e.g., antennabeams 481 may include elliptical beams and/or shaped beams of variousdifferent shapes).

It should be noted that in one or more embodiments, the payload antenna480 may comprise one or more reflector dishes including, but not limitedto, parabolic reflectors and/or shaped reflectors. In some embodiments,the payload antenna 480 may comprise one or more multifeed antennaarrays.

The payload 405 transmits 491 unencrypted host telemetry (i.e.unencrypted host TLM, which is telemetry data related to the portion ofthe payload 405 that is utilized by the host SOC 450) to the firstcommunication security module 462. The first communication securitymodule 462 then encrypts the unencrypted host telemetry utilizing thefirst COMSEC variety to generate encrypted host telemetry (i.e.encrypted host TLM).

The payload 405 transmits 492 unencrypted hosted telemetry (i.e.unencrypted HoP TLM, which is telemetry data related to the portion ofthe payload 405 that is leased by the HOC 460) to the secondcommunication security module 465. The second communication securitymodule 465 then encrypts the unencrypted hosted telemetry utilizing thesecond COMSEC variety to generate encrypted hosted telemetry (i.e.encrypted HoP TLM).

The first communication security module 462 then transmits 493 theencrypted host telemetry to a host telemetry transmitter 489. The hosttelemetry transmitter 489 then transmits 495 the encrypted hosttelemetry to the host SOC 450. The host telemetry transmitter 489transmits 495 the encrypted host telemetry utilizing an out-of-bandfrequency band(s). The host SOC 450 then decrypts the encrypted hosttelemetry utilizing the first COMSEC variety to generate the unencryptedhost telemetry.

The second communication security module 465 then transmits 496 theencrypted hosted telemetry to a hosted telemetry transmitter 494. Thehosted telemetry transmitter 494 then transmits 498 the encrypted hostedtelemetry to the host SOC 450. The telemetry transmitter 494 transmits498 the encrypted hosted telemetry utilizing an out-of-band frequencyband(s). The host SOC 450 then transmits 499 the encrypted hostedtelemetry to the HOC 460. The HOC 460 then decrypts the encrypted hostedtelemetry utilizing the second COMSEC variety to generate theunencrypted hosted telemetry.

FIGS. 5A, 5B, 5C, and 5D together show a flow chart for the disclosedmethod for a virtual transponder utilizing inband commanding for thehost user, in accordance with at least one embodiment of the presentdisclosure. At the start 500 of the method, a hosted payload (HoP)operation center (HOC) encrypts unencrypted hosted commands by utilizinga second communication security (COMSEC) variety to produce encryptedhosted commands 505. Then, the HOC transmits the encrypted hostedcommands to a host spacecraft operations center (SOC) 510. The host SOCthen transmits the encrypted hosted commands to a vehicle 515. Then, ahosted command receiver on the vehicle receives the encrypted hostedcommands 520. The hosted command receiver then transmits the encryptedhosted commands to a second communication security module 525.

Then, the host SOC encrypts unencrypted host commands by utilizing afirst COMSEC variety to produce encrypted host commands 530. The hostSOC then transmits the encrypted host commands to a host receivingantenna 535. Then, the host receiving antenna transmits the encryptedhost commands to a payload antenna on the vehicle 540. The payloadantenna then transmits the encrypted host commands to a payload on thevehicle 545. Then, the payload transmits the encrypted host commands toa first communication security module 550. The first communicationsecurity module then decrypts the encrypted host commands utilizing thefirst COMSEC variety to generate the unencrypted host commands 555. Thesecond communication security module decrypts the encrypted hostedcommands utilizing the second COMSEC variety to generate the unencryptedhosted commands 560. Then, the first communication security moduletransmits the unencrypted host commands to the payload 565. The secondcommunication security module transmits the unencrypted hosted commandsto the payload 570.

Then, the payload is reconfigured according to the unencrypted hostcommands and/or the unencrypted hosted commands 575. The payload antennathen transmits payload data to the host receiving antenna and/or ahosted receiving antenna 580. Then, the payload transmits to the firstcommunication security module unencrypted host telemetry 585. Thepayload transmits to the second communication security moduleunencrypted hosted telemetry 590. Then, the first communication securitymodule encrypts the unencrypted host telemetry utilizing the firstCOMSEC variety to generate encrypted host telemetry 591. The secondcommunication security module encrypts the unencrypted hosted telemetryutilizing the second COMSEC variety to generate encrypted hostedtelemetry 592.

Then, the first communication security module transmits the encryptedhost telemetry to a host telemetry transmitter 593. The host telemetrytransmitter then transmits the encrypted host telemetry to the host SOC594. Then, the host SOC decrypts the encrypted host telemetry utilizingthe first COMSEC variety to generate the unencrypted host telemetry 595.

Then, the second communication security module transmits the encryptedhosted telemetry to a hosted telemetry transmitter 596. The hostedtelemetry transmitter then transmits the encrypted hosted telemetry tothe host SOC 597. Then, the host SOC transmits the encrypted hostedtelemetry to the HOC 598. The HOC then decrypts the encrypted hostedtelemetry utilizing the second COMSEC variety to generate theunencrypted hosted telemetry 599. Then, the method ends 501.

FIG. 6A is a diagram 600 showing the disclosed system for a virtualtransponder utilizing inband commanding for the host user (i.e. hostSOC) 650 and the hosted user (i.e. HOC) 660 using two receiving antennasand employing two communication security (COMSEC) varieties fortelemetry, in accordance with at least one embodiment of the presentdisclosure. In this figure, a vehicle 610, a host SOC 650, and a HOC 660are shown. The HOC 660 has leased at least a portion (e.g., a virtualtransponder(s)) of the payload 605 of the vehicle 610 from the owner ofa satellite (i.e. the host SOC) 650. It should be noted that in someembodiments, the HOC 660 may lease all of the payload 605 of the vehicle610 from the owner of a satellite (i.e. the host SOC) 650. Also, itshould be noted that is some embodiments, the HOC 660 may own thepayload 605 (e.g., a steerable antenna) of the vehicle 610, and contractthe host SOC 650 to transmit encrypted hosted commands to the vehicle610.

During operation, the HOC 660 encrypts unencrypted hosted commands (i.e.unencrypted HoP CMD), by utilizing a second COMSEC variety, to produceencrypted hosted commands (i.e. encrypted HoP CMD). The hosted commandsare commands that are used to configure the portion (e.g., a virtualtransponder(s)) of the payload 605 that the HOC 660 is leasing from thehost SOC 650. The host SOC 650 encrypts unencrypted host commands (i.e.unencrypted host CMD), by utilizing a first COMSEC variety, to produceencrypted host commands (i.e. encrypted host CMD). The host commands arecommands that are used to configure the portion (e.g., a transponder(s))of the payload 605 that host SOC 650 is utilizing for itself.

It should be noted that, although in FIG. 6A the host SOC 650 isdepicted to have its ground antenna located right next to its operationsbuilding; in other embodiments, the host SOC 650 may have its groundantenna located very far away from the its operations building (e.g.,the ground antenna may be located in another country than the operationsbuilding).

Also, it should be noted that the first COMSEC variety may include atleast one encryption key and/or at least one algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm). Additionally, itshould be noted that the second COMSEC variety may include at least oneencryption key and/or at least one encryption algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm).

The host SOC 650 then transmits 620 the encrypted host commands to ahost receiving antenna 685. After the host receiving antenna 685receives the encrypted host commands, the host receiving antenna 685transmits 621 the encrypted host commands to a payload antenna 680 onthe vehicle 610. The host receiving antenna 685 transmits 621 theencrypted host commands utilizing an in-band frequency band(s) (i.e. afrequency band(s) that is the same frequency band(s) utilized totransmit payload data). The payload antenna 680 transmits the encryptedhost commands to a payload 605. The payload 605 on the vehicle 610receives the encrypted host commands. The payload 605 then transmits 652the encrypted host commands to a first communication security module662. The first communication security module 662 decrypts the encryptedhost commands utilizing the first COMSEC variety (i.e. COMSEC Variety 1)to generate unencrypted host commands.

It should be noted that the first communication security module 662 maycomprise one or more modules. In addition, the first communicationsecurity module 662 may comprise one or more processors.

The HOC 660 then transmits 615 the encrypted hosted commands to a hostedreceiving antenna 690. After the hosted receiving antenna 690 receivesthe encrypted hosted commands, the hosted receiving antenna 690transmits 697 the encrypted hosted commands to a payload antenna 680 onthe vehicle 610. The hosted receiving antenna 690 transmits 697 theencrypted hosted commands utilizing an in-band frequency band(s) (i.e. afrequency band(s) that is the same frequency band(s) utilized totransmit payload data). The payload antenna 680 transmits the encryptedhosted commands to a payload 605. The payload 605 on the vehicle 610receives the encrypted hosted commands. The payload 605 then transmits655 the encrypted hosted commands to a second communication securitymodule 665. The second communication security module 665 decrypts theencrypted hosted commands utilizing the second COMSEC variety (i.e.COMSEC Variety 2) to generate unencrypted hosted commands.

It should be noted that the second communication security module 665 maycomprise one or more modules. In addition, the second communicationsecurity module 665 may comprise one or more processors.

The first communication security module 662 then transmits 670 theunencrypted host commands to the payload (i.e. the shared host/hostedpayload) 605. The second communication security module 665 transmits 675the unencrypted hosted commands to the payload (i.e. the sharedhost/hosted payload) 605. The payload 605 is reconfigured according tothe unencrypted host commands and/or the unencrypted hosted commands.The payload antenna 680 then transmits (e.g., in one or more antennabeams 681) payload data to the host receiving antenna 685 and/or thehosted receiving antenna 690 on the ground.

Also, it should be noted that, although in FIG. 6A, antenna beams 681 isshown to include a plurality of circular spot beams; in otherembodiments, antenna beams 681 may include more or less number of beamsthan is shown in FIG. 6A (e.g., antenna beams 681 may only include asingle beam), and antenna beams 681 may include beams of differentshapes than circular spot beams as is shown in FIG. 6A (e.g., antennabeams 681 may include elliptical beams and/or shaped beams of variousdifferent shapes).

It should be noted that in one or more embodiments, the payload antenna680 may comprise one or more reflector dishes including, but not limitedto, parabolic reflectors and/or shaped reflectors. In some embodiments,the payload antenna 680 may comprise one or more multifeed antennaarrays.

The payload 605 transmits 691 unencrypted host telemetry (i.e.unencrypted host TLM, which is telemetry data related to the portion ofthe payload 605 that is utilized by the host SOC 650) to the firstcommunication security module 662. The first communication securitymodule 662 then encrypts the unencrypted host telemetry utilizing thefirst COMSEC variety to generate encrypted host telemetry (i.e.encrypted host TLM).

The payload 605 transmits 692 unencrypted hosted telemetry (i.e.unencrypted HoP TLM, which is telemetry data related to the portion ofthe payload 605 that is leased by the HOC 660) to the secondcommunication security module 665. The second communication securitymodule 665 then encrypts the unencrypted hosted telemetry utilizing thesecond COMSEC variety to generate encrypted hosted telemetry (i.e.encrypted HoP TLM).

The first communication security module 662 then transmits 693 theencrypted host telemetry to a host telemetry transmitter 689. The hosttelemetry transmitter 689 then transmits 695 the encrypted hosttelemetry to the host SOC 650. The host telemetry transmitter 689transmits 695 the encrypted host telemetry utilizing an out-of-bandfrequency band(s). The host SOC 650 then decrypts the encrypted hosttelemetry utilizing the first COMSEC variety to generate the unencryptedhost telemetry.

The second communication security module 665 then transmits 696 theencrypted hosted telemetry to a hosted telemetry transmitter 694. Thehosted telemetry transmitter 694 then transmits 698 the encrypted hostedtelemetry to the host SOC 650. The telemetry transmitter 694 transmits698 the encrypted hosted telemetry utilizing an out-of-band frequencyband(s). The host SOC 650 then transmits 699 the encrypted hostedtelemetry to the HOC 660. The HOC 660 then decrypts the encrypted hostedtelemetry utilizing the second COMSEC variety to generate theunencrypted hosted telemetry.

FIG. 6B is a diagram 6000 showing the disclosed system for a virtualtransponder utilizing inband commanding for the host user (i.e. hostSOC) 6050 and the hosted user (i.e. HOC) 6060 using one receivingantenna and employing two communication security (COMSEC) varieties fortelemetry, in accordance with at least one embodiment of the presentdisclosure. In this figure, a vehicle 6010, a host SOC 6050, and a HOC6060 are shown. The HOC 6060 has leased at least a portion (e.g., avirtual transponder(s)) of the payload 6005 of the vehicle 6010 from theowner of a satellite (i.e. the host SOC) 6050. It should be noted thatin some embodiments, the HOC 6060 may lease all of the payload 6005 ofthe vehicle 6010 from the owner of a satellite (i.e. the host SOC) 6050.Also, it should be noted that is some embodiments, the HOC 6060 may ownthe payload 6005 (e.g., a steerable antenna) of the vehicle 6010, andcontract the host SOC 6050 to transmit encrypted hosted commands to thevehicle 6010.

During operation, the HOC 6060 encrypts unencrypted hosted commands(i.e. unencrypted HoP CMD), by utilizing a second COMSEC variety, toproduce encrypted hosted commands (i.e. encrypted HoP CMD). The hostedcommands are commands that are used to configure the portion (e.g., avirtual transponder(s)) of the payload 6005 that the HOC 6060 is leasingfrom the host SOC 6050. The host SOC 6050 encrypts unencrypted hostcommands (i.e. unencrypted host CMD), by utilizing a first COMSECvariety, to produce encrypted host commands (i.e. encrypted host CMD).The host commands are commands that are used to configure the portion(e.g., a transponder(s)) of the payload 6005 that host SOC 6050 isutilizing for itself.

It should be noted that, although in FIG. 6B the host SOC 6050 isdepicted to have its ground antenna located right next to its operationsbuilding; in other embodiments, the host SOC 6050 may have its groundantenna located very far away from the its operations building (e.g.,the ground antenna may be located in another country than the operationsbuilding).

Also, it should be noted that the first COMSEC variety may include atleast one encryption key and/or at least one algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm). Additionally, itshould be noted that the second COMSEC variety may include at least oneencryption key and/or at least one encryption algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm).

The HOC 6060 transmits 6015 the encrypted hosted commands to the hostSOC 6050. The host SOC 6050 then transmits 6020, 6025 the encrypted hostcommands and the encrypted hosted commands to a host receiving antenna6085. After the host receiving antenna 6085 receives the encrypted hostcommands and the encrypted hosted commands, the host receiving antenna6085 transmits 6097, 6021 the encrypted host commands and the encryptedhosted commands to a payload antenna 6080 on the vehicle 6010. The hostreceiving antenna 6085 transmits 6097, 6021 the encrypted host commandsand the encrypted hosted commands utilizing an in-band frequency band(s)(i.e. a frequency band(s) that is the same frequency band(s) utilized totransmit payload data). The payload antenna 6080 transmits the encryptedhost commands and the encrypted hosted commands to a payload 6005. Thepayload 6005 on the vehicle 6010 receives the encrypted host commandsand the encrypted hosted commands. The payload 6005 then transmits 6052the encrypted host commands to a first communication security module6062. The first communication security module 6062 decrypts theencrypted host commands utilizing the first COMSEC variety (i.e. COMSECVariety 1) to generate unencrypted host commands.

It should be noted that the first communication security module 6062 maycomprise one or more modules. In addition, the first communicationsecurity module 6062 may comprise one or more processors.

The payload 6005 then transmits 6055 the encrypted hosted commands to asecond communication security module 6065. The second communicationsecurity module 6065 decrypts the encrypted hosted commands utilizingthe second COMSEC variety (i.e. COMSEC Variety 2) to generateunencrypted hosted commands.

It should be noted that the second communication security module 6065may comprise one or more modules. In addition, the second communicationsecurity module 6065 may comprise one or more processors.

The first communication security module 6062 then transmits 6070 theunencrypted host commands to the payload (i.e. the shared host/hostedpayload) 6005. The second communication security module 6065 transmits6075 the unencrypted hosted commands to the payload (i.e. the sharedhost/hosted payload) 6005. The payload 6005 is reconfigured according tothe unencrypted host commands and/or the unencrypted hosted commands.The payload antenna 6080 then transmits (e.g., in one or more antennabeams 6081) payload data to a host receiving antenna 6085 and/or thehosted receiving antenna 6090 on the ground.

Also, it should be noted that, although in FIG. 6B, antenna beams 6081is shown to include a plurality of circular spot beams; in otherembodiments, antenna beams 6081 may include more or less number of beamsthan is shown in FIG. 6B (e.g., antenna beams 6081 may only include asingle beam), and antenna beams 6081 may include beams of differentshapes than circular spot beams as is shown in FIG. 6B (e.g., antennabeams 6081 may include elliptical beams and/or shaped beams of variousdifferent shapes).

It should be noted that in one or more embodiments, the payload antenna6080 may comprise one or more reflector dishes including, but notlimited to, parabolic reflectors and/or shaped reflectors. In someembodiments, the payload antenna 6080 may comprise one or more multifeedantenna arrays.

The payload 6005 transmits 6091 unencrypted host telemetry (i.e.unencrypted host TLM, which is telemetry data related to the portion ofthe payload 6005 that is utilized by the host SOC 6050) to the firstcommunication security module 6062. The first communication securitymodule 6062 then encrypts the unencrypted host telemetry utilizing thefirst COMSEC variety to generate encrypted host telemetry (i.e.encrypted host TLM).

The payload 6005 transmits 6092 unencrypted hosted telemetry (i.e.unencrypted HoP TLM, which is telemetry data related to the portion ofthe payload 6005 that is leased by the HOC 6060) to the secondcommunication security module 6065. The second communication securitymodule 6065 then encrypts the unencrypted hosted telemetry utilizing thesecond COMSEC variety to generate encrypted hosted telemetry (i.e.encrypted HoP TLM).

The first communication security module 6062 then transmits 6093 theencrypted host telemetry to a host telemetry transmitter 6089. The hosttelemetry transmitter 6089 then transmits 6095 the encrypted hosttelemetry to the host SOC 6050. The host telemetry transmitter 6089transmits 6095 the encrypted host telemetry utilizing an out-of-bandfrequency band(s). The host SOC 6050 then decrypts the encrypted hosttelemetry utilizing the first COMSEC variety to generate the unencryptedhost telemetry.

The second communication security module 6065 then transmits 6096 theencrypted hosted telemetry to a hosted telemetry transmitter 6094. Thehosted telemetry transmitter 6094 then transmits 6098 the encryptedhosted telemetry to the host SOC 6050. The telemetry transmitter 6094transmits 6098 the encrypted hosted telemetry utilizing an out-of-bandfrequency band(s). The host SOC 6050 then transmits 6099 the encryptedhosted telemetry to the HOC 6060. The HOC 6060 then decrypts theencrypted hosted telemetry utilizing the second COMSEC variety togenerate the unencrypted hosted telemetry.

FIGS. 7A, 7B, 7C, and 7D together show a flow chart for the disclosedmethod for a virtual transponder utilizing inband commanding for thehost user and the hosted user using two receiving antennas and employingtwo COMSEC varieties for telemetry, in accordance with at least oneembodiment of the present disclosure. At the start 700 of the method, ahosted payload (HoP) operation center (HOC) encrypts unencrypted hostedcommands by utilizing a second communication security (COMSEC) varietyto produce encrypted hosted commands 705. Then, the HOC transmits theencrypted hosted commands to a hosted receiving antenna 710. The hostedreceiving antenna then transmits the encrypted hosted commands to apayload antenna on a vehicle 715. Then, the payload antenna transmitsthe encrypted hosted commands to a payload on the vehicle 720. Thepayload then transmits the encrypted hosted commands to a secondcommunication security module 725.

Then, a host spacecraft operations center (SOC) encrypts unencryptedhost commands by utilizing a first COMSEC variety to produce encryptedhost commands 730. The host SOC then transmits the encrypted hostcommands to a host receiving antenna 735. Then, the host receivingantenna transmits the encrypted host commands to a payload antenna onthe vehicle 740. The payload antenna then transmits the encrypted hostcommands to the payload 745. Then, the payload transmits the encryptedhost commands to a first communication security module 750. The firstcommunication security module then decrypts the encrypted host commandsutilizing the first COMSEC variety to generate the unencrypted hostcommands 755. The second communication security module decrypts theencrypted hosted commands utilizing the second COMSEC variety togenerate the unencrypted hosted commands 760. Then, the firstcommunication security module transmits the unencrypted host commands tothe payload 765. The second communication security module then transmitsthe unencrypted hosted commands to the payload 770.

Then, the payload is reconfigured according to the unencrypted hostcommands and/or the unencrypted hosted commands 775. The payload antennathen transmits payload data to the host receiving antenna and/or thehosted receiving antenna 780. Then, the payload transmits to the firstcommunication security module unencrypted host telemetry 785. Thepayload then transmits to the second communication security moduleunencrypted hosted telemetry 790. Then, the first communication securitymodule encrypts the unencrypted host telemetry utilizing the firstCOMSEC variety to generate encrypted host telemetry 791. The secondcommunication security module encrypts the unencrypted hosted telemetryutilizing the second COMSEC variety to generate encrypted hostedtelemetry 792.

Then, the first communication security module transmits the encryptedhost telemetry to a host telemetry transmitter 793. The host telemetrytransmitter then transmits the encrypted host telemetry to the host SOC794. Then, the host SOC decrypts the encrypted host telemetry utilizingthe first COMSEC variety to generate the unencrypted host telemetry 795.

Then, the second communication security module transmits the encryptedhosted telemetry to a hosted telemetry transmitter 796. The hostedtelemetry transmitter then transmits the encrypted hosted telemetry tothe host SOC 797. Then, the host SOC transmits the encrypted hostedtelemetry to the HOC 798. The HOC then decrypts the encrypted hostedtelemetry utilizing the second COMSEC variety to generate theunencrypted hosted telemetry 799. Then, the method ends 701.

FIGS. 7E, 7F, 7G, and 7H together show a flow chart for the disclosedmethod for a virtual transponder utilizing inband commanding for thehost user and the hosted user using one receiving antenna and employingtwo communication security (COMSEC) varieties for telemetry, inaccordance with at least one embodiment of the present disclosure. Atthe start 70000 of the method, a hosted payload (HoP) operation center(HOC) encrypts unencrypted hosted commands by utilizing a secondcommunication security (COMSEC) variety to produce encrypted hostedcommands 70005. Then, the HOC transmits the encrypted hosted commands toa host spacecraft operations center (SOC) 70010. The host SOC encryptsunencrypted host commands by utilizing a first COMSEC variety to produceencrypted host commands 70015. The host SOC then transmits the encryptedhost commands and the encrypted hosted commands to a host receivingantenna 70020. Then, the host receiving antenna transmits the encryptedhost commands and the encrypted hosted commands to a payload antenna onthe vehicle 70025. The payload antenna then transmits the encrypted hostcommands and the encrypted hosted commands to a payload on the vehicle70030. Then, the payload transmits the encrypted host commands to afirst communication security module 70035. The payload then transmitsthe encrypted hosted commands to a second communication security module70040.

The first communication security module then decrypts the encrypted hostcommands utilizing the first COMSEC variety to generate the unencryptedhost commands 70045. The second communication security module decryptsthe encrypted hosted commands utilizing the second COMSEC variety togenerate the unencrypted hosted commands 70050. Then, the firstcommunication security module transmits the unencrypted host commands tothe payload 70055. The second communication security module transmitsthe unencrypted hosted commands to the payload 70060.

Then, the payload is reconfigured according to the unencrypted hostcommands and/or the unencrypted hosted commands 70065. The payloadantenna then transmits payload data to the host receiving antenna and/ora hosted receiving antenna 70070. Then, the payload transmits to thefirst communication security module unencrypted host telemetry 70075.The payload transmits to the second communication security moduleunencrypted hosted telemetry 70080. Then, the first communicationsecurity module encrypts the unencrypted host telemetry utilizing thefirst COMSEC variety to generate encrypted host telemetry 70085. Thesecond communication security module encrypts the unencrypted hostedtelemetry utilizing the second COMSEC variety to generate encryptedhosted telemetry 70090.

Then, the first communication security module transmits the encryptedhost telemetry to a host telemetry transmitter 70091. The host telemetrytransmitter then transmits the encrypted host telemetry to the host SOC70092. Then, the host SOC decrypts the encrypted host telemetryutilizing the first COMSEC variety to generate the unencrypted hosttelemetry 70093.

Then, the second communication security module transmits the encryptedhosted telemetry to a hosted telemetry transmitter 70094. The hostedtelemetry transmitter then transmits the encrypted hosted telemetry tothe host SOC 70095. Then, the host SOC transmits the encrypted hostedtelemetry to the HOC 70096. The HOC then decrypts the encrypted hostedtelemetry utilizing the second COMSEC variety to generate theunencrypted hosted telemetry 70097. Then, the method ends 70098.

FIG. 8A is a diagram 800 showing the disclosed system for a virtualtransponder utilizing inband commanding for the host user (i.e. hostSOC) 850 and the hosted user (i.e. HOC) 860 using two receiving antennasand employing one COMSEC variety for telemetry, in accordance with atleast one embodiment of the present disclosure. In this figure, avehicle 810, a host SOC 850, and a HOC 860 are shown. The HOC 860 hasleased at least a portion (e.g., a virtual transponder(s)) of thepayload 805 of the vehicle 810 from the owner of a satellite (i.e. thehost SOC) 850. It should be noted that in some embodiments, the HOC 860may lease all of the payload 805 of the vehicle 810 from the owner of asatellite (i.e. the host SOC) 850. Also, it should be noted that is someembodiments, the HOC 860 may own the payload 805 (e.g., a steerableantenna) of the vehicle 810, and contract the host SOC 850 to transmitencrypted hosted commands to the vehicle 810.

During operation, the HOC 860 encrypts unencrypted hosted commands (i.e.unencrypted HoP CMD), by utilizing a second COMSEC variety, to produceencrypted hosted commands (i.e. encrypted HoP CMD). The hosted commandsare commands that are used to configure the portion (e.g., a virtualtransponder(s)) of the payload 805 that the HOC 860 is leasing from thehost SOC 850. The host SOC 850 encrypts unencrypted host commands (i.e.unencrypted host CMD), by utilizing a first COMSEC variety, to produceencrypted host commands (i.e. encrypted host CMD). The host commands arecommands that are used to configure the portion (e.g., a transponder(s))of the payload 805 that host SOC 850 is utilizing for itself.

It should be noted that, although in FIG. 8A the host SOC 850 isdepicted to have its ground antenna located right next to its operationsbuilding; in other embodiments, the host SOC 850 may have its groundantenna located very far away from the its operations building (e.g.,the ground antenna may be located in another country than the operationsbuilding).

Also, it should be noted that the first COMSEC variety may include atleast one encryption key and/or at least one algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm). Additionally, itshould be noted that the second COMSEC variety may include at least oneencryption key and/or at least one encryption algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm).

The host SOC 850 then transmits 820 the encrypted host commands to ahost receiving antenna 885. After the host receiving antenna 885receives the encrypted host commands, the host receiving antenna 885transmits 821 the encrypted host commands to a payload antenna 880 onthe vehicle 810. The host receiving antenna 885 transmits 821 theencrypted host commands utilizing an in-band frequency band(s) (i.e. afrequency band(s) that is the same frequency band(s) utilized totransmit payload data). The payload antenna 880 transmits the encryptedhost commands to a payload 805. The payload 805 on the vehicle 810receives the encrypted host commands. The payload 805 then transmits 852the encrypted host commands to a first communication security module862. The first communication security module 862 decrypts the encryptedhost commands utilizing the first COMSEC variety (i.e. COMSEC Variety 1)to generate unencrypted host commands.

It should be noted that the first communication security module 862 maycomprise one or more modules. In addition, the first communicationsecurity module 862 may comprise one or more processors.

The HOC 860 then transmits 815 the encrypted hosted commands to a hostedreceiving antenna 890. After the hosted receiving antenna 890 receivesthe encrypted hosted commands, the hosted receiving antenna 890transmits 897 the encrypted hosted commands to a payload antenna 880 onthe vehicle 810. The hosted receiving antenna 890 transmits 897 theencrypted hosted commands utilizing an in-band frequency band(s) (i.e. afrequency band(s) that is the same frequency band(s) utilized totransmit payload data). The payload antenna 880 transmits the encryptedhosted commands to a payload 805. The payload 805 on the vehicle 810receives the encrypted hosted commands. The payload 805 then transmits855 the encrypted hosted commands to a second communication securitymodule 865. The second communication security module 865 decrypts theencrypted hosted commands utilizing the second COMSEC variety (i.e.COMSEC Variety 2) to generate unencrypted hosted commands.

It should be noted that the second communication security module 865 maycomprise one or more modules. In addition, the second communicationsecurity module 865 may comprise one or more processors.

The first communication security module 862 then transmits 870 theunencrypted host commands to the payload (i.e. the shared host/hostedpayload) 805. The second communication security module 865 transmits 875the unencrypted hosted commands to the payload (i.e. the sharedhost/hosted payload) 805. The payload 805 is reconfigured according tothe unencrypted host commands and/or the unencrypted hosted commands.The payload antenna 880 then transmits (e.g., in one or more antennabeams 881) payload data to the host receiving antenna 885 and/or thehosted receiving antenna 890 on the ground.

Also, it should be noted that, although in FIG. 8A, antenna beams 881 isshown to include a plurality of circular spot beams; in otherembodiments, antenna beams 881 may include more or less number of beamsthan is shown in FIG. 8A (e.g., antenna beams 881 may only include asingle beam), and antenna beams 881 may include beams of differentshapes than circular spot beams as is shown in FIG. 8A (e.g., antennabeams 881 may include elliptical beams and/or shaped beams of variousdifferent shapes).

It should be noted that in one or more embodiments, the payload antenna880 may comprise one or more reflector dishes including, but not limitedto, parabolic reflectors and/or shaped reflectors. In some embodiments,the payload antenna 880 may comprise one or more multifeed antennaarrays.

The payload 805 transmits 891 unencrypted telemetry (i.e. unencryptedhost TLM, which is telemetry data related to the portion of the payload805 that is utilized by the host SOC 850; and unencrypted HoP TLM, whichis telemetry data related to the portion of the payload 805 that isleased by the HOC 860) to the first communication security module 862.The first communication security module 862 then encrypts theunencrypted telemetry utilizing the first COMSEC variety to generateencrypted telemetry (i.e. encrypted TLM).

The first communication security module 862 then transmits 893 theencrypted telemetry to a telemetry transmitter 889. The telemetrytransmitter 889 then transmits 895 the encrypted telemetry to the hostSOC 850. The host telemetry transmitter 889 transmits 895 the encryptedtelemetry utilizing an out-of-band frequency band(s).

The host SOC 850 then decrypts the encrypted telemetry utilizing thefirst COMSEC variety to generate the unencrypted telemetry. The host SOC850 then utilizes a database that comprises host payload decommutatedinformation and does not comprise hosted payload decommutatedinformation (i.e. a database without hosted payload decommutatedinformation) to read to unencrypted telemetry to determine the telemetrydata related to the portion of the payload 805 that is utilized by thehost SOC 850.

The host SOC 850 then transmits 899 the encrypted telemetry to the HOC860. The HOC 860 then decrypts the encrypted telemetry utilizing thefirst COMSEC variety to generate the unencrypted telemetry. The HOC 860then utilizes a database that comprises hosted payload decommutatedinformation and does not comprise host payload decommutated information(i.e. a database without host payload decommutated information) to readto unencrypted telemetry to determine the telemetry data related to theportion of the payload 805 that is utilized by the HOC 860.

FIG. 8B is a diagram 8000 showing the disclosed system for a virtualtransponder utilizing inband commanding for the host user (i.e. hostSOC) 8050 and the hosted user (i.e. HOC) 8060 using one receivingantenna and employing one COMSEC variety for telemetry, in accordancewith at least one embodiment of the present disclosure. In this figure,a vehicle 8010, a host SOC 8050, and a HOC 8060 are shown. The HOC 8060has leased at least a portion (e.g., a virtual transponder(s)) of thepayload 8005 of the vehicle 8010 from the owner of a satellite (i.e. thehost SOC) 8050. It should be noted that in some embodiments, the HOC8060 may lease all of the payload 8005 of the vehicle 8010 from theowner of a satellite (i.e. the host SOC) 8050. Also, it should be notedthat is some embodiments, the HOC 8060 may own the payload 8005 (e.g., asteerable antenna) of the vehicle 8010, and contract the host SOC 8050to transmit encrypted hosted commands to the vehicle 8010.

During operation, the HOC 8060 encrypts unencrypted hosted commands(i.e. unencrypted HoP CMD), by utilizing a second COMSEC variety, toproduce encrypted hosted commands (i.e. encrypted HoP CMD). The hostedcommands are commands that are used to configure the portion (e.g., avirtual transponder(s)) of the payload 8005 that the HOC 8060 is leasingfrom the host SOC 8050. The host SOC 8050 encrypts unencrypted hostcommands (i.e. unencrypted host CMD), by utilizing a first COMSECvariety, to produce encrypted host commands (i.e. encrypted host CMD).The host commands are commands that are used to configure the portion(e.g., a transponder(s)) of the payload 8005 that host SOC 8050 isutilizing for itself.

It should be noted that, although in FIG. 8B the host SOC 8050 isdepicted to have its ground antenna located right next to its operationsbuilding; in other embodiments, the host SOC 8050 may have its groundantenna located very far away from the its operations building (e.g.,the ground antenna may be located in another country than the operationsbuilding).

Also, it should be noted that the first COMSEC variety may include atleast one encryption key and/or at least one algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm). Additionally, itshould be noted that the second COMSEC variety may include at least oneencryption key and/or at least one encryption algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm).

The host SOC 8050 then transmits 8020 the encrypted host commands to ahost receiving antenna 8085. After the host receiving antenna 8085receives the encrypted host commands, the host receiving antenna 8085transmits 8021 the encrypted host commands to a payload antenna 8080 onthe vehicle 8010. The host receiving antenna 8085 transmits 8021 theencrypted host commands utilizing an in-band frequency band(s) (i.e. afrequency band(s) that is the same frequency band(s) utilized totransmit payload data). The payload antenna 8080 transmits the encryptedhost commands to a payload 8005. The payload 8005 on the vehicle 8010receives the encrypted host commands. The payload 8005 then transmits8052 the encrypted host commands to a first communication securitymodule 8062. The first communication security module 8062 decrypts theencrypted host commands utilizing the first COMSEC variety (i.e. COMSECVariety 1) to generate unencrypted host commands.

It should be noted that the first communication security module 8062 maycomprise one or more modules. In addition, the first communicationsecurity module 8062 may comprise one or more processors.

The HOC 8060 then transmits 8015 the encrypted hosted commands to thehost SOC 8050. The host SOC 8050 then transmits 8016 the encryptedhosted commands to a host receiving antenna 8085. After the hostreceiving antenna 8085 receives the encrypted hosted commands, the hostreceiving antenna 8085 transmits 8097 the encrypted hosted commands to apayload antenna 8080 on the vehicle 8010. The host receiving antenna8085 transmits 8097 the encrypted hosted commands utilizing an in-bandfrequency band(s) (i.e. a frequency band(s) that is the same frequencyband(s) utilized to transmit payload data). The payload antenna 8080transmits the encrypted hosted commands to a payload 8005. The payload8005 on the vehicle 8010 receives the encrypted hosted commands. Thepayload 8005 then transmits 8055 the encrypted hosted commands to asecond communication security module 8065. The second communicationsecurity module 8065 decrypts the encrypted hosted commands utilizingthe second COMSEC variety (i.e. COMSEC Variety 2) to generateunencrypted hosted commands.

It should be noted that the second communication security module 8065may comprise one or more modules. In addition, the second communicationsecurity module 8065 may comprise one or more processors.

The first communication security module 8062 then transmits 8070 theunencrypted host commands to the payload (i.e. the shared host/hostedpayload) 8005. The second communication security module 8065 transmits8075 the unencrypted hosted commands to the payload (i.e. the sharedhost/hosted payload) 8005. The payload 8005 is reconfigured according tothe unencrypted host commands and/or the unencrypted hosted commands.The payload antenna 8080 then transmits (e.g., in one or more antennabeams 8081) payload data to the host receiving antenna 8085 and/or thehosted receiving antenna 8090 on the ground.

Also, it should be noted that, although in FIG. 8B, antenna beams 8081is shown to include a plurality of circular spot beams; in otherembodiments, antenna beams 8081 may include more or less number of beamsthan is shown in FIG. 8B (e.g., antenna beams 8081 may only include asingle beam), and antenna beams 8081 may include beams of differentshapes than circular spot beams as is shown in FIG. 8B (e.g., antennabeams 8081 may include elliptical beams and/or shaped beams of variousdifferent shapes).

It should be noted that in one or more embodiments, the payload antenna8080 may comprise one or more reflector dishes including, but notlimited to, parabolic reflectors and/or shaped reflectors. In someembodiments, the payload antenna 8080 may comprise one or more multifeedantenna arrays.

The payload 8005 transmits 8091 unencrypted telemetry (i.e. unencryptedhost TLM, which is telemetry data related to the portion of the payload8005 that is utilized by the host SOC 8050; and unencrypted HoP TLM,which is telemetry data related to the portion of the payload 8005 thatis leased by the HOC 8060) to the first communication security module8062. The first communication security module 8062 then encrypts theunencrypted telemetry utilizing the first COMSEC variety to generateencrypted telemetry (i.e. encrypted TLM).

The first communication security module 8062 then transmits 8093 theencrypted telemetry to a telemetry transmitter 8089. The telemetrytransmitter 8089 then transmits 8095 the encrypted telemetry to the hostSOC 8050. The host telemetry transmitter 8089 transmits 8095 theencrypted telemetry utilizing an out-of-band frequency band(s).

The host SOC 8050 then decrypts the encrypted telemetry utilizing thefirst COMSEC variety to generate the unencrypted telemetry. The host SOC8050 then utilizes a database that comprises host payload decommutatedinformation and does not comprise hosted payload decommutatedinformation (i.e. a database without hosted payload decommutatedinformation) to read to unencrypted telemetry to determine the telemetrydata related to the portion of the payload 8005 that is utilized by thehost SOC 8050.

The host SOC 8050 then transmits 8099 the encrypted telemetry to the HOC8060. The HOC 8060 then decrypts the encrypted telemetry utilizing thefirst COMSEC variety to generate the unencrypted telemetry. The HOC 8060then utilizes a database that comprises hosted payload decommutatedinformation and does not comprise host payload decommutated information(i.e. a database without host payload decommutated information) to readto unencrypted telemetry to determine the telemetry data related to theportion of the payload 8005 that is utilized by the HOC 8060.

FIGS. 9A, 9B, 9C, and 9D together show a flow chart for the disclosedmethod for a virtual transponder utilizing inband commanding for thehost user and the hosted user using two receiving antennas and employingone COMSEC variety for telemetry, in accordance with at least oneembodiment of the present disclosure. At the start 900 of the method, ahosted payload (HoP) operation center (HOC) encrypts unencrypted hostedcommands by utilizing a second communication security (COMSEC) varietyto produce encrypted hosted commands 905. Then, the HOC transmits theencrypted hosted commands to a hosted receiving antenna 910. The hostedreceiving antenna then transmits the encrypted hosted commands to apayload antenna on a vehicle 915. Then, the payload antenna transmitsthe encrypted hosted commands to a payload on the vehicle 920. Thepayload then transmits the encrypted hosted commands to a secondcommunication security module 925.

Then, a host spacecraft operations center (SOC) encrypts unencryptedhost commands by utilizing a first COMSEC variety to produce encryptedhost commands 930. The host SOC then transmits the encrypted hostcommands to a host receiving antenna 935. Then, the host receivingantenna transmits the encrypted host commands to a payload antenna onthe vehicle 940. The payload antenna then transmits the encrypted hostcommands to the payload 945. Then, the payload transmits the encryptedhost commands to a first communication security module 950. The firstcommunication security module then decrypts the encrypted host commandsutilizing the first COMSEC variety to generate the unencrypted hostcommands 955. Then, the second communication security module decryptsthe encrypted hosted commands utilizing the second COMSEC variety togenerate the unencrypted hosted commands 960. The first communicationsecurity module then transmits the unencrypted host commands to thepayload 965. Then, the second communication security module transmitsthe unencrypted hosted commands to the payload 970.

Then, the payload is reconfigured according to the unencrypted hostcommands and/or the unencrypted hosted commands 975. The payload antennathen transmits payload data to the host receiving antenna and/or thehosted receiving antenna 980. Then, the payload transmits to the firstcommunication security module unencrypted telemetry 985. The firstcommunication security module then encrypts the unencrypted telemetryutilizing the first COMSEC variety to generate encrypted telemetry 990.

Then, the first communication security module transmits the encryptedtelemetry to a telemetry transmitter 991. The telemetry transmitter thentransmits the encrypted telemetry to the host SOC 992. Then, the hostSOC decrypts the encrypted telemetry utilizing the first COMSEC varietyto generate the unencrypted host telemetry 993. The host SOC thendetermining telemetry data related to a portion of the payload utilizedby the host SOC by using a database without hosted decommutatedinformation to read the unencrypted telemetry 994. Then, the host SOCtransmits the encrypted telemetry to the HOC 995. The HOC then decryptsthe encrypted telemetry utilizing the first COMSEC variety to generatethe unencrypted telemetry 996. Then, the HOC determines telemetry datarelated to a portion of the payload utilized by the HOC by using adatabase without host decommutated information to read the unencryptedtelemetry 997. Then, the method ends 998.

FIGS. 9E, 9F, 9G, and 9H together show a flow chart for the disclosedmethod for a virtual transponder utilizing inband commanding for thehost user and the hosted user using one receiving antenna and employingone COMSEC variety for telemetry, in accordance with at least oneembodiment of the present disclosure. At the start 9000 of the method, ahosted payload (HoP) operation center (HOC) encrypts unencrypted hostedcommands by utilizing a second communication security (COMSEC) varietyto produce encrypted hosted commands 9005. Then, the HOC transmits theencrypted hosted commands to a host spacecraft operations center (SOC)9010. The host SOC then transmits the encrypted hosted commands to ahost receiving antenna 9012. The host receiving antenna then transmitsthe encrypted hosted commands to a payload antenna on a vehicle 9015.Then, the payload antenna transmits the encrypted hosted commands to apayload on the vehicle 9020. The payload then transmits the encryptedhosted commands to a second communication security module 9025.

Then, a host spacecraft operations center (SOC) encrypts unencryptedhost commands by utilizing a first COMSEC variety to produce encryptedhost commands 9030. The host SOC then transmits the encrypted hostcommands to a host receiving antenna 9035. Then, the host receivingantenna transmits the encrypted host commands to a payload antenna onthe vehicle 9040. The payload antenna then transmits the encrypted hostcommands to the payload 9045. Then, the payload transmits the encryptedhost commands to a first communication security module 9050. The firstcommunication security module then decrypts the encrypted host commandsutilizing the first COMSEC variety to generate the unencrypted hostcommands 9055. Then, the second communication security module decryptsthe encrypted hosted commands utilizing the second COMSEC variety togenerate the unencrypted hosted commands 9060. The first communicationsecurity module then transmits the unencrypted host commands to thepayload 9065. Then, the second communication security module transmitsthe unencrypted hosted commands to the payload 9070.

Then, the payload is reconfigured according to the unencrypted hostcommands and/or the unencrypted hosted commands 9075. The payloadantenna then transmits payload data to the host receiving antenna and/orthe hosted receiving antenna 9080. Then, the payload transmits to thefirst communication security module unencrypted telemetry 9085. Thefirst communication security module then encrypts the unencryptedtelemetry utilizing the first COMSEC variety to generate encryptedtelemetry 9090.

Then, the first communication security module transmits the encryptedtelemetry to a telemetry transmitter 9091. The telemetry transmitterthen transmits the encrypted telemetry to the host SOC 9092. Then, thehost SOC decrypts the encrypted telemetry utilizing the first COMSECvariety to generate the unencrypted host telemetry 9093. The host SOCthen determining telemetry data related to a portion of the payloadutilized by the host SOC by using a database without hosted decommutatedinformation to read the unencrypted telemetry 9094. Then, the host SOCtransmits the encrypted telemetry to the HOC 9095. The HOC then decryptsthe encrypted telemetry utilizing the first COMSEC variety to generatethe unencrypted telemetry 9096. Then, the HOC determines telemetry datarelated to a portion of the payload utilized by the HOC by using adatabase without host decommutated information to read the unencryptedtelemetry 9097. Then, the method ends 9098.

FIG. 10A is a diagram 1000 showing the disclosed system for a virtualtransponder utilizing inband telemetry and commanding for the host user(i.e. host SOC) 1050 and the hosted user (i.e. HOC) 1060 using tworeceiving antennas and employing two COMSEC varieties for telemetry, inaccordance with at least one embodiment of the present disclosure. Inthis figure, a vehicle 1010, a host SOC 1050, and a HOC 1060 are shown.The HOC 1060 has leased at least a portion (e.g., a virtualtransponder(s)) of the payload 1005 of the vehicle 1010 from the ownerof a satellite (i.e. the host SOC) 1050. It should be noted that in someembodiments, the HOC 1060 may lease all of the payload 1005 of thevehicle 1010 from the owner of a satellite (i.e. the host SOC) 1050.Also, it should be noted that is some embodiments, the HOC 1060 may ownthe payload 1005 (e.g., a steerable antenna) of the vehicle 1010, andcontract the host SOC 1050 to transmit encrypted hosted commands to thevehicle 1010.

During operation, the HOC 1060 encrypts unencrypted hosted commands(i.e. unencrypted HoP CMD), by utilizing a second COMSEC variety, toproduce encrypted hosted commands (i.e. encrypted HoP CMD). The hostedcommands are commands that are used to configure the portion (e.g., avirtual transponder(s)) of the payload 1005 that the HOC 1060 is leasingfrom the host SOC 1050. The host SOC 1050 encrypts unencrypted hostcommands (i.e. unencrypted host CMD), by utilizing a first COMSECvariety, to produce encrypted host commands (i.e. encrypted host CMD).The host commands are commands that are used to configure the portion(e.g., a transponder(s)) of the payload 1005 that host SOC 1050 isutilizing for itself.

It should be noted that, although in FIG. 10A the host SOC 1050 isdepicted to have its ground antenna located right next to its operationsbuilding; in other embodiments, the host SOC 1050 may have its groundantenna located very far away from the its operations building (e.g.,the ground antenna may be located in another country than the operationsbuilding).

Also, it should be noted that the first COMSEC variety may include atleast one encryption key and/or at least one algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm). Additionally, itshould be noted that the second COMSEC variety may include at least oneencryption key and/or at least one encryption algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm).

The host SOC 1050 then transmits 1020 the encrypted host commands to ahost receiving antenna 1085. After the host receiving antenna 1085receives the encrypted host commands, the host receiving antenna 1085transmits 1021 the encrypted host commands to a payload antenna 1080 onthe vehicle 1010. The host receiving antenna 1085 transmits 1021 theencrypted host commands utilizing an in-band frequency band(s) (i.e. afrequency band(s) that is the same frequency band(s) utilized totransmit payload data). The payload antenna 1080 transmits the encryptedhost commands to a payload 1005. The payload 1005 on the vehicle 1010receives the encrypted host commands. The payload 1005 then transmits1052 the encrypted host commands to a first communication securitymodule 1062. The first communication security module 1062 decrypts theencrypted host commands utilizing the first COMSEC variety (i.e. COMSECVariety 1) to generate unencrypted host commands.

It should be noted that the first communication security module 1062 maycomprise one or more modules. In addition, the first communicationsecurity module 1062 may comprise one or more processors.

The HOC 1060 then transmits 1015 the encrypted hosted commands to ahosted receiving antenna 1090. After the hosted receiving antenna 1090receives the encrypted hosted commands, the hosted receiving antenna1090 transmits 1097 the encrypted hosted commands to a payload antenna1080 on the vehicle 1010. The hosted receiving antenna 1090 transmits1097 the encrypted hosted commands utilizing an in-band frequencyband(s) (i.e. a frequency band(s) that is the same frequency band(s)utilized to transmit payload data). The payload antenna 1080 transmitsthe encrypted hosted commands to a payload 1005. The payload 1005 on thevehicle 1010 receives the encrypted hosted commands. The payload 1005then transmits 1055 the encrypted hosted commands to a secondcommunication security module 1065. The second communication securitymodule 1065 decrypts the encrypted hosted commands utilizing the secondCOMSEC variety (i.e. COMSEC Variety 2) to generate unencrypted hostedcommands.

It should be noted that the second communication security module 1065may comprise one or more modules. In addition, the second communicationsecurity module 1065 may comprise one or more processors.

The first communication security module 1062 then transmits 1070 theunencrypted host commands to the payload (i.e. the shared host/hostedpayload) 1005. The second communication security module 1065 transmits1075 the unencrypted hosted commands to the payload (i.e. the sharedhost/hosted payload) 1005. The payload 1005 is reconfigured according tothe unencrypted host commands and/or the unencrypted hosted commands.The payload antenna 1080 then transmits (e.g., in one or more antennabeams 1081) payload data to the host receiving antenna 1085 and/or thehosted receiving antenna 1090 on the ground.

Also, it should be noted that, although in FIG. 10A, antenna beams 1081is shown to include a plurality of circular spot beams; in otherembodiments, antenna beams 1081 may include more or less number of beamsthan is shown in FIG. 10A (e.g., antenna beams 1081 may only include asingle beam), and antenna beams 1081 may include beams of differentshapes than circular spot beams as is shown in FIG. 10A (e.g., antennabeams 1081 may include elliptical beams and/or shaped beams of variousdifferent shapes).

It should be noted that in one or more embodiments, the payload antenna1080 may comprise one or more reflector dishes including, but notlimited to, parabolic reflectors and/or shaped reflectors. In someembodiments, the payload antenna 1080 may comprise one or more multifeedantenna arrays.

The payload 1005 transmits 1091 unencrypted host telemetry (i.e.unencrypted host TLM, which is telemetry data related to the portion ofthe payload 1005 that is utilized by the host SOC 1050) to the firstcommunication security module 1062. The first communication securitymodule 1062 then encrypts the unencrypted host telemetry utilizing thefirst COMSEC variety to generate encrypted host telemetry (i.e.encrypted host TLM).

The payload 1005 transmits 1092 unencrypted hosted telemetry (i.e.unencrypted HoP TLM, which is telemetry data related to the portion ofthe payload 1005 that is leased by the HOC 1060) to the secondcommunication security module 1065. The second communication securitymodule 1065 then encrypts the unencrypted hosted telemetry utilizing thesecond COMSEC variety to generate encrypted hosted telemetry (i.e.encrypted HoP TLM).

The first communication security module 1062 then transmits 1093 theencrypted host telemetry to the payload 1005. The payload 1005 thentransmits the encrypted host telemetry to the payload antenna 1080. Thepayload antenna 1080 transmits 1095 the encrypted host telemetry to thehost receiving antenna 1085. The payload antenna 1080 transmits 1095 theencrypted host telemetry utilizing an in-band frequency band(s). Thehost receiving antenna 1085 then transmits 1094 the encrypted hosttelemetry to the host SOC 1050. The host SOC 1050 then decrypts theencrypted host telemetry utilizing the first COMSEC variety to generatethe unencrypted host telemetry.

The second communication security module 1065 then transmits 1096 theencrypted hosted telemetry to the payload 1005. The payload 1005 thentransmits the encrypted hosted telemetry to the payload antenna 1080.The payload antenna 1080 transmits 1098 the encrypted hosted telemetryto the hosted receiving antenna 1090. The payload antenna 1080 transmits1098 the encrypted hosted telemetry utilizing an in-band frequencyband(s). The hosted receiving antenna 1090 then transmits 1099 theencrypted hosted telemetry to the HOC 1060. The HOC 1060 then decryptsthe encrypted hosted telemetry utilizing the second COMSEC variety togenerate the unencrypted hosted telemetry.

FIG. 10B is a diagram 10000 showing the disclosed system for a virtualtransponder utilizing inband telemetry and commanding for the host user(i.e. host SOC) 10050 and the hosted user (i.e. HOC) 10060 using onereceiving antenna and employing two COMSEC varieties for telemetry, inaccordance with at least one embodiment of the present disclosure. Inthis figure, a vehicle 10010, a host SOC 10050, and a HOC 10060 areshown. The HOC 10060 has leased at least a portion (e.g., a virtualtransponder(s)) of the payload 10005 of the vehicle 10010 from the ownerof a satellite (i.e. the host SOC) 10050. It should be noted that insome embodiments, the HOC 10060 may lease all of the payload 10005 ofthe vehicle 10010 from the owner of a satellite (i.e. the host SOC)10050. Also, it should be noted that is some embodiments, the HOC 10060may own the payload 10005 (e.g., a steerable antenna) of the vehicle10010, and contract the host SOC 10050 to transmit encrypted hostedcommands to the vehicle 10010.

During operation, the HOC 10060 encrypts unencrypted hosted commands(i.e. unencrypted HoP CMD), by utilizing a second COMSEC variety, toproduce encrypted hosted commands (i.e. encrypted HoP CMD). The hostedcommands are commands that are used to configure the portion (e.g., avirtual transponder(s)) of the payload 10005 that the HOC 10060 isleasing from the host SOC 10050. The host SOC 10050 encrypts unencryptedhost commands (i.e. unencrypted host CMD), by utilizing a first COMSECvariety, to produce encrypted host commands (i.e. encrypted host CMD).The host commands are commands that are used to configure the portion(e.g., a transponder(s)) of the payload 10005 that host SOC 10050 isutilizing for itself.

It should be noted that, although in FIG. 10B the host SOC 10050 isdepicted to have its ground antenna located right next to its operationsbuilding; in other embodiments, the host SOC 10050 may have its groundantenna located very far away from the its operations building (e.g.,the ground antenna may be located in another country than the operationsbuilding).

Also, it should be noted that the first COMSEC variety may include atleast one encryption key and/or at least one algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm). Additionally, itshould be noted that the second COMSEC variety may include at least oneencryption key and/or at least one encryption algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm).

The host SOC 10050 then transmits 10020 the encrypted host commands to ahost receiving antenna 10085. After the host receiving antenna 10085receives the encrypted host commands, the host receiving antenna 10085transmits 10021 the encrypted host commands to a payload antenna 10080on the vehicle 10010. The host receiving antenna 10085 transmits 10021the encrypted host commands utilizing an in-band frequency band(s) (i.e.a frequency band(s) that is the same frequency band(s) utilized totransmit payload data). The payload antenna 10080 transmits theencrypted host commands to a payload 10005. The payload 10005 on thevehicle 10010 receives the encrypted host commands. The payload 10005then transmits 10052 the encrypted host commands to a firstcommunication security module 10062. The first communication securitymodule 10062 decrypts the encrypted host commands utilizing the firstCOMSEC variety (i.e. COMSEC Variety 1) to generate unencrypted hostcommands.

It should be noted that the first communication security module 10062may comprise one or more modules. In addition, the first communicationsecurity module 10062 may comprise one or more processors.

The HOC 10060 then transmits 10015 the encrypted hosted commands to thehost SOC 10050. The host SOC 10050 then transmits 10087 the encryptedhosted commands to the host receiving antenna 10085. After the hostreceiving antenna 10085 receives the encrypted hosted commands, the hostreceiving antenna 10085 transmits 10097 the encrypted hosted commands toa payload antenna 10080 on the vehicle 10010. The host receiving antenna10085 transmits 10097 the encrypted hosted commands utilizing an in-bandfrequency band(s) (i.e. a frequency band(s) that is the same frequencyband(s) utilized to transmit payload data). The payload antenna 10080transmits the encrypted hosted commands to a payload 10005. The payload10005 on the vehicle 10010 receives the encrypted hosted commands. Thepayload 10005 then transmits 10055 the encrypted hosted commands to asecond communication security module 10065. The second communicationsecurity module 10065 decrypts the encrypted hosted commands utilizingthe second COMSEC variety (i.e. COMSEC Variety 2) to generateunencrypted hosted commands.

It should be noted that the second communication security module 10065may comprise one or more modules. In addition, the second communicationsecurity module 10065 may comprise one or more processors.

The first communication security module 10062 then transmits 10070 theunencrypted host commands to the payload (i.e. the shared host/hostedpayload) 10005. The second communication security module 10065 transmits10075 the unencrypted hosted commands to the payload (i.e. the sharedhost/hosted payload) 10005. The payload 10005 is reconfigured accordingto the unencrypted host commands and/or the unencrypted hosted commands.The payload antenna 10080 then transmits (e.g., in one or more antennabeams 10081) payload data to the host receiving antenna 10085 and/or thehosted receiving antenna 10090 on the ground.

Also, it should be noted that, although in FIG. 10B, antenna beams 10081is shown to include a plurality of circular spot beams; in otherembodiments, antenna beams 10081 may include more or less number ofbeams than is shown in FIG. 10B (e.g., antenna beams 10081 may onlyinclude a single beam), and antenna beams 10081 may include beams ofdifferent shapes than circular spot beams as is shown in FIG. 10B (e.g.,antenna beams 10081 may include elliptical beams and/or shaped beams ofvarious different shapes).

It should be noted that in one or more embodiments, the payload antenna10080 may comprise one or more reflector dishes including, but notlimited to, parabolic reflectors and/or shaped reflectors. In someembodiments, the payload antenna 10080 may comprise one or moremultifeed antenna arrays.

The payload 10005 transmits 10091 unencrypted host telemetry (i.e.unencrypted host TLM, which is telemetry data related to the portion ofthe payload 10005 that is utilized by the host SOC 10050) to the firstcommunication security module 10062. The first communication securitymodule 10062 then encrypts the unencrypted host telemetry utilizing thefirst COMSEC variety to generate encrypted host telemetry (i.e.encrypted host TLM).

The payload 10005 transmits 10092 unencrypted hosted telemetry (i.e.unencrypted HoP TLM, which is telemetry data related to the portion ofthe payload 10005 that is leased by the HOC 10060) to the secondcommunication security module 10065. The second communication securitymodule 10065 then encrypts the unencrypted hosted telemetry utilizingthe second COMSEC variety to generate encrypted hosted telemetry (i.e.encrypted HoP TLM).

The first communication security module 10062 then transmits 10093 theencrypted host telemetry to the payload 10005. The payload 10005 thentransmits the encrypted host telemetry to the payload antenna 10080. Thepayload antenna 10080 transmits 10095 the encrypted host telemetry tothe host receiving antenna 10085. The payload antenna 10080 transmits10095 the encrypted host telemetry utilizing an in-band frequencyband(s). The host receiving antenna 10085 then transmits 10094 theencrypted host telemetry to the host SOC 10050. The host SOC 10050 thendecrypts the encrypted host telemetry utilizing the first COMSEC varietyto generate the unencrypted host telemetry.

The second communication security module 10065 then transmits 10096 theencrypted hosted telemetry to the payload 10005. The payload 10005 thentransmits the encrypted hosted telemetry to the payload antenna 10080.The payload antenna 10080 transmits 10098 the encrypted hosted telemetryto the host receiving antenna 10085. The payload antenna 10080 transmits10098 the encrypted hosted telemetry utilizing an in-band frequencyband(s). The host receiving antenna 10085 then transmits 10086 theencrypted hosted telemetry to the host SOC 10050. The host SOC 10050then transmits 10099 the encrypted hosted telemetry to the HOC 10060.The HOC 10060 then decrypts the encrypted hosted telemetry utilizing thesecond COMSEC variety to generate the unencrypted hosted telemetry.

FIGS. 11A, 11B, 11C, and 11D together show a flow chart for thedisclosed method for a virtual transponder utilizing inband telemetryand commanding for the host user and the hosted user using two receivingantennas and employing two COMSEC varieties for telemetry, in accordancewith at least one embodiment of the present disclosure. At the start1100 of the method, a hosted payload (HoP) operation center (HOC)encrypts unencrypted hosted commands by utilizing a second communicationsecurity (COMSEC) variety to produce encrypted hosted commands 1105.Then, the HOC transmits the encrypted hosted commands to a hostedreceiving antenna 1110. The hosted receiving antenna then transmits theencrypted hosted commands to a payload antenna on a vehicle 1115. Then,the payload antenna transmits the encrypted hosted commands to a payloadon the vehicle 1120. The payload then transmits the encrypted hostedcommands to a second communication security module 1125.

Then, a host spacecraft operations center (SOC) encrypts unencryptedhost commands by utilizing a first COMSEC variety to produce encryptedhost commands 1130. The host SOC then transmits the encrypted hostcommands to a host receiving antenna 1135. Then, the host receivingantenna transmits the encrypted host commands to the payload antenna1140. The payload antenna then transmits the encrypted host commands tothe payload 1145. Then, the payload transmits the encrypted hostcommands to a first communication security module 1150. The firstcommunication security module then decrypts the encrypted host commandsutilizing the first COMSEC variety to generate the unencrypted hostcommands 1155. Then, the second communication security module decryptsthe encrypted hosted commands utilizing the second COMSEC variety togenerate the unencrypted hosted commands 1160. Then, the firstcommunication security module transmits the unencrypted host commands tothe payload 1165. The second communication security module thentransmits the unencrypted hosted commands to the payload 1170.

Then, the payload is reconfigured according to the unencrypted hostcommands and/or the unencrypted hosted commands 1175. The payloadantenna then transmits payload data to the host receiving antenna and/orthe hosted receiving antenna 1180. Then, the payload transmits to thefirst communication security module unencrypted host telemetry 1185. Thepayload then transmits to the second communication security moduleunencrypted hosted telemetry 1190. Then, the first communicationsecurity module encrypts the unencrypted host telemetry utilizing thefirst COMSEC variety to generate encrypted host telemetry 1191. Thesecond communication security module then encrypts the unencryptedhosted telemetry utilizing the second COMSEC variety to generateencrypted hosted telemetry 1192.

Then, the first communication security module transmits the encryptedhost telemetry to the payload 1193. The payload then transmits theencrypted host telemetry to the payload antenna 1194. Then, the payloadantenna transmits the encrypted host telemetry to the host receivingantenna 1195. The host receiving antenna transmits the encrypted hosttelemetry to the host SOC 1196. Then, the host SOC decrypts theencrypted host telemetry utilizing the first COMSEC variety to generatethe unencrypted host telemetry 1197.

Then, the second communication security module transmits the encryptedhosted telemetry to the payload 1198. The payload then transmits theencrypted hosted telemetry to the payload antenna 1199. Then, thepayload antenna transmits the encrypted hosted telemetry to the hostedreceiving antenna 1101. The hosted receiving antenna transmits theencrypted hosted telemetry to the HOC 1102. Then, the HOC decrypts theencrypted hosted telemetry utilizing the second COMSEC variety togenerate the unencrypted hosted telemetry 1103. Then, the method ends1104.

FIGS. 11E, 11F, 11G, and 11H together show a flow chart for thedisclosed method for a virtual transponder utilizing inband telemetryand commanding for the host user and the hosted user using one receivingantenna and employing two COMSEC varieties for telemetry, in accordancewith at least one embodiment of the present disclosure. At the start11000 of the method, a hosted payload (HoP) operation center (HOC)encrypts unencrypted hosted commands by utilizing a second communicationsecurity (COMSEC) variety to produce encrypted hosted commands 11005.Then, the HOC transmits the encrypted hosted commands to a hostspacecraft operations center (SOC) 11010. The host SOC then transmitsthe encrypted hosted commands to a host receiving antenna 11012. Thehost receiving antenna then transmits the encrypted hosted commands to apayload antenna on a vehicle 11015. Then, the payload antenna transmitsthe encrypted hosted commands to a payload on the vehicle 11020. Thepayload then transmits the encrypted hosted commands to a secondcommunication security module 11025.

Then, a host spacecraft operations center (SOC) encrypts unencryptedhost commands by utilizing a first COMSEC variety to produce encryptedhost commands 11030. The host SOC then transmits the encrypted hostcommands to a host receiving antenna 11035. Then, the host receivingantenna transmits the encrypted host commands to the payload antenna11040. The payload antenna then transmits the encrypted host commands tothe payload 11045. Then, the payload transmits the encrypted hostcommands to a first communication security module 11050. The firstcommunication security module then decrypts the encrypted host commandsutilizing the first COMSEC variety to generate the unencrypted hostcommands 11055. Then, the second communication security module decryptsthe encrypted hosted commands utilizing the second COMSEC variety togenerate the unencrypted hosted commands 11060. Then, the firstcommunication security module transmits the unencrypted host commands tothe payload 11065. The second communication security module thentransmits the unencrypted hosted commands to the payload 11070.

Then, the payload is reconfigured according to the unencrypted hostcommands and/or the unencrypted hosted commands 11075. The payloadantenna then transmits payload data to the host receiving antenna and/orthe hosted receiving antenna 11080. Then, the payload transmits to thefirst communication security module unencrypted host telemetry 11085.The payload then transmits to the second communication security moduleunencrypted hosted telemetry 11090. Then, the first communicationsecurity module encrypts the unencrypted host telemetry utilizing thefirst COMSEC variety to generate encrypted host telemetry 11091. Thesecond communication security module then encrypts the unencryptedhosted telemetry utilizing the second COMSEC variety to generateencrypted hosted telemetry 11092.

Then, the first communication security module transmits the encryptedhost telemetry to the payload 11093. The payload then transmits theencrypted host telemetry to the payload antenna 11094. Then, the payloadantenna transmits the encrypted host telemetry to the host receivingantenna 11095. The host receiving antenna transmits the encrypted hosttelemetry to the host SOC 11096. Then, the host SOC decrypts theencrypted host telemetry utilizing the first COMSEC variety to generatethe unencrypted host telemetry 11097.

Then, the second communication security module transmits the encryptedhosted telemetry to the payload 11098. The payload then transmits theencrypted hosted telemetry to the payload antenna 11099. Then, thepayload antenna transmits the encrypted hosted telemetry to the hostreceiving antenna 11001. The host receiving antenna transmits theencrypted hosted telemetry to the host SOC 11002. The host SOC thentransmits the encrypted hosted telemetry to the HOC 11003. Then, the HOCdecrypts the encrypted hosted telemetry utilizing the second COMSECvariety to generate the unencrypted hosted telemetry 11004. Then, themethod ends 11005.

FIG. 12A is a diagram 1200 showing the disclosed system for a virtualtransponder utilizing inband telemetry and commanding for the host user(i.e. host SOC) 1250 and the hosted user (i.e. HOC) 1260 using tworeceiving antennas and employing one COMSEC variety for telemetry, inaccordance with at least one embodiment of the present disclosure. Inthis figure, a vehicle 1210, a host SOC 1250, and a HOC 1260 are shown.The HOC 1260 has leased at least a portion (e.g., a virtualtransponder(s)) of the payload 1205 of the vehicle 1210 from the ownerof a satellite (i.e. the host SOC) 1250. It should be noted that in someembodiments, the HOC 1260 may lease all of the payload 1205 of thevehicle 1210 from the owner of a satellite (i.e. the host SOC) 1250.Also, it should be noted that is some embodiments, the HOC 1260 may ownthe payload 1205 (e.g., a steerable antenna) of the vehicle 1210, andcontract the host SOC 1250 to transmit encrypted hosted commands to thevehicle 1210.

During operation, the HOC 1260 encrypts unencrypted hosted commands(i.e. unencrypted HoP CMD), by utilizing a second COMSEC variety, toproduce encrypted hosted commands (i.e. encrypted HoP CMD). The hostedcommands are commands that are used to configure the portion (e.g., avirtual transponder(s)) of the payload 1205 that the HOC 1260 is leasingfrom the host SOC 1250. The host SOC 1250 encrypts unencrypted hostcommands (i.e. unencrypted host CMD), by utilizing a first COMSECvariety, to produce encrypted host commands (i.e. encrypted host CMD).The host commands are commands that are used to configure the portion(e.g., a transponder(s)) of the payload 1205 that host SOC 1250 isutilizing for itself.

It should be noted that, although in FIG. 12A the host SOC 1250 isdepicted to have its ground antenna located right next to its operationsbuilding; in other embodiments, the host SOC 1250 may have its groundantenna located very far away from the its operations building (e.g.,the ground antenna may be located in another country than the operationsbuilding).

Also, it should be noted that the first COMSEC variety may include atleast one encryption key and/or at least one algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm). Additionally, itshould be noted that the second COMSEC variety may include at least oneencryption key and/or at least one encryption algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm).

The host SOC 1250 then transmits 1220 the encrypted host commands to ahost receiving antenna 1285. After the host receiving antenna 1285receives the encrypted host commands, the host receiving antenna 1285transmits 1221 the encrypted host commands to a payload antenna 1280 onthe vehicle 1210. The host receiving antenna 1285 transmits 1221 theencrypted host commands utilizing an in-band frequency band(s) (i.e. afrequency band(s) that is the same frequency band(s) utilized totransmit payload data). The payload antenna 1280 transmits the encryptedhost commands to a payload 1205. The payload 1205 on the vehicle 1210receives the encrypted host commands. The payload 1205 then transmits1252 the encrypted host commands to a first communication securitymodule 1262. The first communication security module 1262 decrypts theencrypted host commands utilizing the first COMSEC variety (i.e. COMSECVariety 1) to generate unencrypted host commands.

It should be noted that the first communication security module 1262 maycomprise one or more modules. In addition, the first communicationsecurity module 1262 may comprise one or more processors.

The HOC 1260 then transmits 1215 the encrypted hosted commands to ahosted receiving antenna 1290. After the hosted receiving antenna 1290receives the encrypted hosted commands, the hosted receiving antenna1290 transmits 1297 the encrypted hosted commands to a payload antenna1280 on the vehicle 1210. The hosted receiving antenna 1290 transmits1297 the encrypted hosted commands utilizing an in-band frequencyband(s) (i.e. a frequency band(s) that is the same frequency band(s)utilized to transmit payload data). The payload antenna 1280 transmitsthe encrypted hosted commands to a payload 1205. The payload 1205 on thevehicle 1210 receives the encrypted hosted commands. The payload 1205then transmits 1255 the encrypted hosted commands to a secondcommunication security module 1265. The second communication securitymodule 1265 decrypts the encrypted hosted commands utilizing the secondCOMSEC variety (i.e. COMSEC Variety 2) to generate unencrypted hostedcommands.

It should be noted that the second communication security module 1265may comprise one or more modules. In addition, the second communicationsecurity module 1265 may comprise one or more processors.

The first communication security module 1262 then transmits 1270 theunencrypted host commands to the payload (i.e. the shared host/hostedpayload) 1205. The second communication security module 1265 transmits1275 the unencrypted hosted commands to the payload (i.e. the sharedhost/hosted payload) 1205. The payload 1205 is reconfigured according tothe unencrypted host commands and/or the unencrypted hosted commands.The payload antenna 1280 then transmits (e.g., in one or more antennabeams 1281) payload data to the host receiving antenna 1285 and/or thehosted receiving antenna 1290 on the ground.

Also, it should be noted that, although in FIG. 12A, antenna beams 1281is shown to include a plurality of circular spot beams; in otherembodiments, antenna beams 1281 may include more or less number of beamsthan is shown in FIG. 12A (e.g., antenna beams 1281 may only include asingle beam), and antenna beams 1281 may include beams of differentshapes than circular spot beams as is shown in FIG. 12A (e.g., antennabeams 1281 may include elliptical beams and/or shaped beams of variousdifferent shapes).

It should be noted that in one or more embodiments, the payload antenna1280 may comprise one or more reflector dishes including, but notlimited to, parabolic reflectors and/or shaped reflectors. In someembodiments, the payload antenna 1280 may comprise one or more multifeedantenna arrays.

The payload 1205 transmits 1291 unencrypted telemetry (i.e. unencryptedhost TLM, which is telemetry data related to the portion of the payload1205 that is utilized by the host SOC 1250; and unencrypted HoP TLM,which is telemetry data related to the portion of the payload 1205 thatis leased by the HOC 1260) to the first communication security module1262. The first communication security module 1262 then encrypts theunencrypted telemetry utilizing the first COMSEC variety to generateencrypted telemetry (i.e. encrypted TLM). The first communicationsecurity module 1262 then transmits 1293 the encrypted telemetry to thepayload 1205. The payload 1205 then transmits the encrypted telemetry tothe payload antenna 1280.

The payload antenna 1280 transmits 1295 the encrypted telemetry to thehost receiving antenna 1285. The payload antenna 1280 transmits 1295 theencrypted telemetry utilizing an in-band frequency band(s). The hostreceiving antenna 1285 then transmits 1294 the encrypted telemetry tothe host SOC 1250. The host SOC 1250 then decrypts the encryptedtelemetry utilizing the first COMSEC variety to generate the unencryptedtelemetry. The host SOC 1250 then utilizes a database that compriseshost payload decommutated information and does not comprise hostedpayload decommutated information (i.e. a database without hosted payloaddecommutated information) to read to unencrypted telemetry to determinethe telemetry data related to the portion of the payload 1205 that isutilized by the host SOC 1250.

The payload antenna 1280 transmits 1298 the encrypted telemetry to thehosted receiving antenna 1290. The payload antenna 1280 transmits 1298the encrypted telemetry utilizing an in-band frequency band(s). Thehosted receiving antenna 1290 then transmits 1299 the encryptedtelemetry to the HOC 1260. The HOC 1260 then decrypts the encryptedtelemetry utilizing the first COMSEC variety to generate the unencryptedtelemetry. The HOC 1260 then utilizes a database that comprises hostedpayload decommutated information and does not comprise host payloaddecommutated information (i.e. a database without host payloaddecommutated information) to read to unencrypted telemetry to determinethe telemetry data related to the portion of the payload 1205 that isutilized by the HOC 1260.

FIG. 12B is a diagram 12000 showing the disclosed system for a virtualtransponder utilizing inband telemetry and commanding for the host user(i.e. host SOC) 12050 and the hosted user (i.e. HOC) 12060 using onereceiving antenna and employing one COMSEC variety for telemetry, inaccordance with at least one embodiment of the present disclosure. Inthis figure, a vehicle 12010, a host SOC 12050, and a HOC 12060 areshown. The HOC 12060 has leased at least a portion (e.g., a virtualtransponder(s)) of the payload 12005 of the vehicle 12010 from the ownerof a satellite (i.e. the host SOC) 12050. It should be noted that insome embodiments, the HOC 12060 may lease all of the payload 12005 ofthe vehicle 12010 from the owner of a satellite (i.e. the host SOC)12050. Also, it should be noted that is some embodiments, the HOC 12060may own the payload 12005 (e.g., a steerable antenna) of the vehicle12010, and contract the host SOC 12050 to transmit encrypted hostedcommands to the vehicle 12010.

During operation, the HOC 12060 encrypts unencrypted hosted commands(i.e. unencrypted HoP CMD), by utilizing a second COMSEC variety, toproduce encrypted hosted commands (i.e. encrypted HoP CMD). The hostedcommands are commands that are used to configure the portion (e.g., avirtual transponder(s)) of the payload 12005 that the HOC 12060 isleasing from the host SOC 12050. The host SOC 12050 encrypts unencryptedhost commands (i.e. unencrypted host CMD), by utilizing a first COMSECvariety, to produce encrypted host commands (i.e. encrypted host CMD).The host commands are commands that are used to configure the portion(e.g., a transponder(s)) of the payload 12005 that host SOC 12050 isutilizing for itself.

It should be noted that, although in FIG. 12B the host SOC 12050 isdepicted to have its ground antenna located right next to its operationsbuilding; in other embodiments, the host SOC 12050 may have its groundantenna located very far away from the its operations building (e.g.,the ground antenna may be located in another country than the operationsbuilding).

Also, it should be noted that the first COMSEC variety may include atleast one encryption key and/or at least one algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm). Additionally, itshould be noted that the second COMSEC variety may include at least oneencryption key and/or at least one encryption algorithm (e.g., a Type 1encryption algorithm or a Type 2 encryption algorithm).

The host SOC 12050 then transmits 12020 the encrypted host commands to ahost receiving antenna 12085. After the host receiving antenna 12085receives the encrypted host commands, the host receiving antenna 12085transmits 12021 the encrypted host commands to a payload antenna 12080on the vehicle 12010. The host receiving antenna 12085 transmits 12021the encrypted host commands utilizing an in-band frequency band(s) (i.e.a frequency band(s) that is the same frequency band(s) utilized totransmit payload data). The payload antenna 12080 transmits theencrypted host commands to a payload 12005. The payload 12005 on thevehicle 12010 receives the encrypted host commands. The payload 12005then transmits 12052 the encrypted host commands to a firstcommunication security module 12062. The first communication securitymodule 12062 decrypts the encrypted host commands utilizing the firstCOMSEC variety (i.e. COMSEC Variety 1) to generate unencrypted hostcommands.

It should be noted that the first communication security module 12062may comprise one or more modules. In addition, the first communicationsecurity module 12062 may comprise one or more processors.

The HOC 12060 then transmits 12015 the encrypted hosted commands to thehost SOC 12050. The host SOC 12050 then transmits 12098 the encryptedhosted commands to the host receiving antenna 12085. After the hostreceiving antenna 12085 receives the encrypted hosted commands, the hostreceiving antenna 12085 transmits 12097 the encrypted hosted commands toa payload antenna 12080 on the vehicle 12010. The host receiving antenna12085 transmits 12097 the encrypted hosted commands utilizing an in-bandfrequency band(s) (i.e. a frequency band(s) that is the same frequencyband(s) utilized to transmit payload data). The payload antenna 12080transmits the encrypted hosted commands to a payload 12005. The payload12005 on the vehicle 12010 receives the encrypted hosted commands. Thepayload 12005 then transmits 12055 the encrypted hosted commands to asecond communication security module 12065. The second communicationsecurity module 12065 decrypts the encrypted hosted commands utilizingthe second COMSEC variety (i.e. COMSEC Variety 2) to generateunencrypted hosted commands.

It should be noted that the second communication security module 12065may comprise one or more modules. In addition, the second communicationsecurity module 12065 may comprise one or more processors.

The first communication security module 12062 then transmits 12070 theunencrypted host commands to the payload (i.e. the shared host/hostedpayload) 12005. The second communication security module 12065 transmits12075 the unencrypted hosted commands to the payload (i.e. the sharedhost/hosted payload) 12005. The payload 12005 is reconfigured accordingto the unencrypted host commands and/or the unencrypted hosted commands.The payload antenna 12080 then transmits (e.g., in one or more antennabeams 12081) payload data to the host receiving antenna 12085 and/or thehosted receiving antenna 12090 on the ground.

Also, it should be noted that, although in FIG. 12B, antenna beams 12081is shown to include a plurality of circular spot beams; in otherembodiments, antenna beams 12081 may include more or less number ofbeams than is shown in FIG. 12B (e.g., antenna beams 12081 may onlyinclude a single beam), and antenna beams 12081 may include beams ofdifferent shapes than circular spot beams as is shown in FIG. 12B (e.g.,antenna beams 12081 may include elliptical beams and/or shaped beams ofvarious different shapes).

It should be noted that in one or more embodiments, the payload antenna12080 may comprise one or more reflector dishes including, but notlimited to, parabolic reflectors and/or shaped reflectors. In someembodiments, the payload antenna 12080 may comprise one or moremultifeed antenna arrays.

The payload 12005 transmits 12091 unencrypted telemetry (i.e.unencrypted host TLM, which is telemetry data related to the portion ofthe payload 12005 that is utilized by the host SOC 12050; andunencrypted HoP TLM, which is telemetry data related to the portion ofthe payload 12005 that is leased by the HOC 12060) to the firstcommunication security module 12062. The first communication securitymodule 12062 then encrypts the unencrypted telemetry utilizing the firstCOMSEC variety to generate encrypted telemetry (i.e. encrypted TLM). Thefirst communication security module 12062 then transmits 12093 theencrypted telemetry to the payload 12005. The payload 12005 thentransmits the encrypted telemetry to the payload antenna 12080.

The payload antenna 12080 transmits 12095 the encrypted telemetry to thehost receiving antenna 12085. The payload antenna 12080 transmits 12095the encrypted telemetry utilizing an in-band frequency band(s). The hostreceiving antenna 12085 then transmits 12094 the encrypted telemetry tothe host SOC 12050. The host SOC 12050 then decrypts the encryptedtelemetry utilizing the first COMSEC variety to generate the unencryptedtelemetry. The host SOC 12050 then utilizes a database that compriseshost payload decommutated information and does not comprise hostedpayload decommutated information (i.e. a database without hosted payloaddecommutated information) to read to unencrypted telemetry to determinethe telemetry data related to the portion of the payload 12005 that isutilized by the host SOC 12050.

The host SOC 12050 then transmits 12099 the encrypted telemetry to theHOC 12060. The HOC 12060 then decrypts the encrypted telemetry utilizingthe first COMSEC variety to generate the unencrypted telemetry. The HOC12060 then utilizes a database that comprises hosted payloaddecommutated information and does not comprise host payload decommutatedinformation (i.e. a database without host payload decommutatedinformation) to read to unencrypted telemetry to determine the telemetrydata related to the portion of the payload 12005 that is utilized by theHOC 12060.

FIGS. 13A, 13B, 13C, and 13D together show a flow chart for thedisclosed method for a virtual transponder utilizing inband telemetryand commanding for the host user and the hosted user using two receivingantennas and employing one COMSEC variety, in accordance with at leastone embodiment of the present disclosure. At the start 1300 of themethod, a hosted payload (HoP) operation center (HOC) encryptsunencrypted hosted commands by utilizing a second communication security(COMSEC) variety to produce encrypted hosted commands 1305. Then, theHOC transmits the encrypted hosted commands to a hosted receivingantenna 1310. The hosted receiving antenna then transmits the encryptedhosted commands to a payload antenna on a vehicle 1315. Then, thepayload antenna transmits the encrypted hosted commands to a payload onthe vehicle 1320. The payload then transmits the encrypted hostedcommands to a second communication security module 1325.

Then, a host spacecraft operations center (SOC) encrypts unencryptedhost commands by utilizing a first COMSEC variety to produce encryptedhost commands 1330. The host SOC then transmits the encrypted hostcommands to a host receiving antenna 1335. Then, the host receivingantenna transmits the encrypted host commands to the payload antenna1340. Then, the payload antenna transmits the encrypted host commands tothe payload 1345. The payload then transmits the encrypted host commandsto a first communication security module 1350. Then, the firstcommunication security module decrypts the encrypted host commandsutilizing the first COMSEC variety to generate the unencrypted hostcommands 1355. The second communication security module then decryptsthe encrypted hosted commands utilizing the second COMSEC variety togenerate the unencrypted hosted commands 1360. Then, the firstcommunication security module transmits the unencrypted host commands tothe payload 1365. The second communication security module thentransmits the unencrypted hosted commands to the payload 1370.

Then, the payload is reconfigured according to the unencrypted hostcommands and/or the unencrypted hosted commands 1375. The payloadantenna then transmits payload data to the host receiving antenna and/orthe hosted receiving antenna 1380. Then, the payload transmits to thefirst communication security module unencrypted telemetry 1385. Thefirst communication security module then encrypts the unencryptedtelemetry utilizing the first COMSEC variety to generate encryptedtelemetry 1390.

Then, the first communication security module transmits the encryptedtelemetry to the payload 1391. The payload then transmits the encryptedtelemetry to the payload antenna 1392. Then, the payload antennatransmits the encrypted telemetry to the host receiving antenna 1393.The host receiving antenna then transmits the encrypted telemetry to thehost SOC 1394. Then, the host SOC decrypts the encrypted telemetryutilizing the first COMSEC variety to generate the unencrypted telemetry1395. The host SOC then determines telemetry data related to a portionof the payload utilized by the host SOC by using a database withouthosted decommutated information to read the unencrypted telemetry 1396.

Then, the payload antenna transmits the encrypted telemetry to thehosted receiving antenna 1397. The hosted receiving antenna thentransmits the encrypted telemetry to the HOC 1398. Then, the HOCdecrypts the encrypted telemetry utilizing the first COMSEC variety togenerate the unencrypted telemetry 1399. The HOC then determinestelemetry data related to a portion of the payload utilized by the HOCby using a database without host decommutated information to read theunencrypted telemetry 1301. Then, the method ends 1302.

FIGS. 13E, 13F, 13G, and 13H together show a flow chart for thedisclosed method for a virtual transponder utilizing inband telemetryand commanding for the host user and the hosted user using one receivingantenna and employing one COMSEC variety, in accordance with at leastone embodiment of the present disclosure. At the start 13000 of themethod, a hosted payload (HoP) operation center (HOC) encryptsunencrypted hosted commands by utilizing a second communication security(COMSEC) variety to produce encrypted hosted commands 13005. Then, theHOC transmits the encrypted hosted commands to a host spacecraftoperations center (SOC) 13010. The host SOC then transmits the encryptedhosted commands to a host receiving antenna 13012. The host receivingantenna then transmits the encrypted hosted commands to a payloadantenna on a vehicle 13015. Then, the payload antenna transmits theencrypted hosted commands to a payload on the vehicle 13020. The payloadthen transmits the encrypted hosted commands to a second communicationsecurity module 13025.

Then, a host spacecraft operations center (SOC) encrypts unencryptedhost commands by utilizing a first COMSEC variety to produce encryptedhost commands 13030. The host SOC then transmits the encrypted hostcommands to a host receiving antenna 13035. Then, the host receivingantenna transmits the encrypted host commands to the payload antenna13040. Then, the payload antenna transmits the encrypted host commandsto the payload 13045. The payload then transmits the encrypted hostcommands to a first communication security module 13050. Then, the firstcommunication security module decrypts the encrypted host commandsutilizing the first COMSEC variety to generate the unencrypted hostcommands 13055. The second communication security module then decryptsthe encrypted hosted commands utilizing the second COMSEC variety togenerate the unencrypted hosted commands 13060. Then, the firstcommunication security module transmits the unencrypted host commands tothe payload 13065. The second communication security module thentransmits the unencrypted hosted commands to the payload 13070.

Then, the payload is reconfigured according to the unencrypted hostcommands and/or the unencrypted hosted commands 13075. The payloadantenna then transmits payload data to the host receiving antenna and/orthe hosted receiving antenna 13080. Then, the payload transmits to thefirst communication security module unencrypted telemetry 13085. Thefirst communication security module then encrypts the unencryptedtelemetry utilizing the first COMSEC variety to generate encryptedtelemetry 13090.

Then, the first communication security module transmits the encryptedtelemetry to the payload 13091. The payload then transmits the encryptedtelemetry to the payload antenna 13092. Then, the payload antennatransmits the encrypted telemetry to the host receiving antenna 13093.The host receiving antenna then transmits the encrypted telemetry to thehost SOC 13094. Then, the host SOC decrypts the encrypted telemetryutilizing the first COMSEC variety to generate the unencrypted telemetry13095. The host SOC then determines telemetry data related to a portionof the payload utilized by the host SOC by using a database withouthosted decommutated information to read the unencrypted telemetry 13096.

The host SOC then transmits the encrypted telemetry to the HOC 13098.Then, the HOC decrypts the encrypted telemetry utilizing the firstCOMSEC variety to generate the unencrypted telemetry 13099. The HOC thendetermines telemetry data related to a portion of the payload utilizedby the HOC by using a database without host decommutated information toread the unencrypted telemetry 13001. Then, the method ends 13002.

FIGS. 14-19B show exemplary systems and methods for a virtualtransponder, in accordance with at least one embodiment of the presentdisclosure.

FIG. 14 is a diagram 1400 showing the disclosed system for a virtualtransponder on a vehicle 1610, in accordance with at least oneembodiment of the present disclosure. In this figure, a computing device1410 is shown. The computing device 1410 may be located at a station(e.g., a host station or a hosted station). When the computing device1410 is located at a host station (i.e. a station operated by a hostuser (Host SOC)), the computing device 1410 is referred to as a hostcomputing device. And, when the computing device 1410 is located at ahosted station (i.e. a station operated by a hosted user (HOC)), thecomputing device 1410 is referred to as a hosted computing device. Inone or more embodiments, the station is a ground station 1415, aterrestrial vehicle (e.g., a military jeep) 1420, an airborne vehicle(e.g., an aircraft) 1425, or a marine vehicle (e.g., a ship) 1430.

During operation, a user (e.g., a host user or a hosted user) 1405selects, via a graphical user interface (GUI) (e.g., a host GUI or ahosted GUI) 1435 displayed on a screen of the computing device 1410(e.g., a host computing device or a hosted computing device), an option(e.g., a value) for each of at least one different variable for aportion of the payload 1680 on the vehicle 1610 utilized by the user1405. It should be noted that the details of payload 1680 as isillustrated in FIG. 16 is depicted on the GUI 1435, which is displayedon the screen of the computing device 1410.

Refer FIG. 16 to view the different variables of the payload 1680 on thevehicle 1610 that may be selected by the user 1405 by using the GUI 1435that is displayed to the user 1405. Also, refer to FIG. 17 to view thedifferent variables of the digital channelizer 1670 of the payload 1680that may be selected by the user 1405 by using the GUI 1435 that isdisplayed to the user 1405. In one or more embodiments, variousdifferent variables may be presented by the GUI 1435 to be selectedincluding, but not limited to, at least one transponder power, at leastone transponder spectrum, at least one transponder gain setting, atleast one transponder limiter setting, at least one transponderautomatic level control setting, at least one transponder phase setting,at least one internal gain generation, bandwidth for at least one beam,at least one frequency band for at least one beam, at least onetransponder beamforming setting, effective isotropic radiation power(EIRP) for at least one beam, at least one transponder channel, and/orbeam steering for at least one beam. It should be noted that the user1405 may select an option by clicking on the associated variable (e.g.,clicking on one of the mixers 1665 to change the frequency band of themixer's associated transmit antenna 1655) in the payload 1680 by usingthe GUI 1435, and by either typing in a value or selecting a value froma drop down menu (e.g., by typing in a desired transmission frequencyband for the associated transmit antenna 1655). It should be noted thatthe payload 1680 depicted in FIG. 16 is an exemplary payload, and thedepiction does not show all possible different variables that may beselected by user 1405 by using the GUI 1435.

After the user 1405 has selected, via the GUI 1435 displayed on thecomputing device 1410, an option for each of at least one variable forthe portion of the payload 1680 on the vehicle 1610 utilized by the user1405, the option(s) is transmitted 1440 to a configuration algorithm(CA) 1445 (e.g., an algorithm contained in an XML file, such asCAConfig.xml 1450). The CA 1445 then generates a configuration for theportion of the payload 1680 on the vehicle 1610 utilized by the user1405 by using the option(s). Then, the CA 1445 transmits 1455 theconfiguration to a command generator (e.g., a host command generator ora hosted command generator) 1460. Optionally, the CA 1445 also storesthe configuration in a report file 1465.

After the command generator 1460 has received the configuration, thecommand generator 1460 generates commands (e.g., host commands or hostedcommands) for reconfiguring the portion of the payload 1680 on thevehicle 1610 utilized by the user 1405 by using the configuration. Then,the commands are transmitted 1470 to an encryption module 1475. Afterreceiving the commands, the encryption module 1475 then encrypts thecommands (e.g., by utilizing a first COMSEC variety or a second COMSECvariety) to generate encrypted commands (e.g., host encrypted commandsor hosted encrypted commands).

Then, the encrypted commands are transmitted 1480 from the station(e.g., a ground station 1415, a terrestrial vehicle (e.g., a militaryjeep) 1420, an airborne vehicle (e.g., an aircraft) 1425, or a marinevehicle (e.g., a ship) 1430) to the vehicle 1410. It should be notedthat, in one or more embodiments, the computing device 1410, the CA1445, the command generator 1460, and the encryption module 1475 are alllocated at the station (e.g., the host station or the hosted station).In other embodiments, some or more of these items may be located indifferent locations. In addition, in one or more embodiments, thevehicle 1610 is an airborne vehicle (e.g., a satellite, an aircraft, anunmanned vehicle (UAV), or a space plane).

After the vehicle 1610 has received the encrypted commands, the vehicledecrypts the commands to generated unencrypted commands (e.g., hostunencrypted commands or hosted unencrypted commands). Then, the portionof the payload 1680 on the vehicle 1610 utilized by the user 1405 isreconfigured by using the unencrypted commands. In one or moreembodiments, the reconfiguring of the payload 1680 may comprisereconfiguring at least one antenna 1615, 1655 (refer to FIG. 16), atleast one analog-to-digital converter, at least one digital-to-analogconverter, at least one beamformer, at least one digital channelizer1710 (refer to FIG. 17), at least one demodulator, at least onemodulator, at least one digital switch matrix 1720 (refer to FIG. 17),and/or at least one digital combiner 1730 (refer to FIG. 17). It shouldbe noted that in other embodiments, the reconfiguring of the payload1680 may comprise reconfiguring at least one analog switch matrix.

FIG. 15 is a diagram 1500 showing an exemplary allocation of bandwidthamongst a plurality of beams (U1-U45) when utilizing the disclosedvirtual transponder, in accordance with at least one embodiment of thepresent disclosure. In this figure, the bandwidth of each of the beams(U1-U45) is illustrated as a bar.

On the left side 1510 of the diagram 1500, a portion of the bandwidth ofeach of the beams (U1-U45) is shown to be utilized by only the host user(i.e. the owner of the vehicle). For this example, the host user is notleasing out any portion of the payload to a hosted user (i.e. acustomer).

On the right side 1520 of the diagram 1500, a portion of the bandwidthof each of the beams is shown to be utilized by the host user (i.e. theowner of the vehicle). Also, at least some (if not all) of the portionof the bandwidth of each of the beams (U1-U45) not utilized by the hostuser, is shown to be utilized by the hosted user (i.e. a customer). Forthis example, the host user is leasing out a portion of the payload to ahosted user (i.e. a customer). Specifically, the host user is leasingout a portion the bandwidth of each of the beams (U1-U45) to the hosteduser.

It should be noted that in other embodiments, the host user may leaseout the entire bandwidth of some (if not all) of beam(s) to the hosteduser. For these, embodiments, the hosted user alone will utilize thebandwidth of these leased beam(s).

FIG. 16 is a diagram 1600 showing the switch architecture for a flexibleallocation of bandwidth amongst a plurality of beams (U1-UN) (i.e.including uplink and downlink beams) when utilizing the disclosedvirtual transponder, in accordance with at least one embodiment of thepresent disclosure. In this figure, details of a payload 1680 on avehicle 1610 are shown. In particular, each of a plurality (i.e. Nnumber) of receive antennas 1615, on the vehicle 1610, is shown to bereceiving one of the uplink beams (U1-UN). As such, for example, receiveantenna 1615 connected to input port 1 receives uplink beam U6, receiveantenna 1615 connected to input port 2 receives uplink beam U14, andreceive antenna 1615 connected to input port N receives uplink beam U34.Each receive antenna 1615 is shown to be followed by a polarizer (i.e.pol) 1620 and a waveguide filter (i.e. WG Filter) 1625.

Also, in this figure, each of a plurality (i.e. N number) of transmitantennas 1655, on the vehicle 1610, is shown to be receiving one of thedownlink beams (U1-UN). As such, for example, transmit antenna 1655connected to output port 1 receives downlink beam U19, transmit antenna1655 connected to output port 2 receives downlink beam U6, and transmitantenna 1655 connected to output port N receives downlink beam U1. Eachtransmit antenna 1655 is shown to be preceded by a polarizer (i.e. pol)1645 and a waveguide filter (i.e. WG Filter) 1650.

It should be noted that, in one or more embodiments, various differenttypes of antennas may be employed for the receive antennas 1615 and thetransmit antennas 1655 including, but not limited to, parabolicreflector antennas, shaped reflector antennas, multifeed array antennas,phase array antennas, and/or any combination thereof.

During operation, a host user 1605 encrypts unencrypted host commands toproduce encrypted host commands. Also, a hosted user 1630 encryptsunencrypted hosted commands to produce encrypted hosted commands. Thehosted user 1630 transmits 1635 the encrypted hosted commands to thehost user 1605. The host user 1605 transmits 1640 the encrypted hostcommands and the encrypted hosted commands to the vehicle 1610. Theencrypted host commands and encrypted hosted commands are decrypted onthe vehicle 1610 to produce the unencrypted host commands andunencrypted hosted commands.

Then, the payload on the vehicle 1610 receives the unencrypted hostcommands and unencrypted hosted commands. The digital channelizer 1670then reconfigures the channels of the uplink beams (U1-UN) and downlinkbeams (U1-UN) according to the unencrypted host commands and unencryptedhosted commands. The configuring of the channels allocates the bandwidthof the uplink beams (U1-UN) and downlink beams (U1-UN) amongst the hostuser 1605 and the hosted user 1630.

Also, the transmit antennas 1655 and the receive antennas 1615 areconfigured according to the unencrypted host commands and/or unencryptedhosted commands. For example, some, if not all, of the transmit antennas1655 and/or the receive antennas 1615 may be gimbaled to project theirbeams on different locations on the ground. Also, for example, some, ifnot all, of the transmit antennas 1655 and/or the receive antennas 1615may have their phase changed such that (1) the shape of the beam ischanged (e.g., has the effect of changing the coverage area of the beam,changing the peak(s) amplitude of the beam, and/or the changing thepeak(s) amplitude location on the ground), and/or (2) the beam isprojected on a different location on the ground (i.e. has the sameeffect as gimbaling the antenna 1615, 1655).

Additionally, the mixers 1660 on the input ports and/or the mixers 1665on the output ports are configured according to the unencrypted hostcommands and/or unencrypted hosted commands. For example, some, if notall, of the mixers 1660 on the input ports and/or the mixers 1665 on theoutput ports may mix in different frequency bands to change thefrequency band(s) of the beams (U1-UN).

FIG. 17 is a diagram 1700 showing details of the digital channelizer1670 of FIG. 16, in accordance with at least one embodiment of thepresent disclosure. In this figure, the digital channelizer 1670 isshown to include three main parts, which are the channelizer 1710, theswitch matrix 1720, and the combiner 1730. The digital channelizer 1710divides the input beam spectrum (i.e. frequency band) from each inputport into input subchannels (i.e. frequency slices). In this figure,each beam spectrum (i.e. frequency band) is shown to be divided intotwelve (12) input subchannels (i.e. frequency slices). It should benoted that in other embodiments, each input beam spectrum may be dividedinto more or less than twelve (12) input subchannels, as is shown inFIG. 17.

The switch matrix 1720 routes the input subchannels from the input portsto their assigned respective output ports, where they are referred to asoutput subchannels. In this figure, five (5) exemplary types of routingthat may be utilized by the switch matrix 1720 are shown, which includedirect mapping 1740, in-beam multicast 1750, cross-beam multicast 1760,cross-beam mapping 1770, and cross-beam point-to-point routing 1780. Thecombiner 1730 combines the output subchannels to create an output beamspectrum for each output port. As previously mentioned above, during thereconfiguring of the payload 1680, the channelizer 1710, the switchmatrix 1720, and/or the combiner 1730 of the digital channelizer 1670may be reconfigured a various different number of ways (e.g., changingthe dividing of the input beam spectrums into input subchannels,changing the routing of the input subchannels, and/or changing thecombining of the output subchannels to create the output beamspectrums).

FIG. 18 is a diagram 1800 showing exemplary components on the vehicle(e.g., satellite) 1810 that may be utilized by the disclosed virtualtransponder, in accordance with at least one embodiment of the presentdisclosure. In this figure, various components, on the vehicle 1810, areshown that may be configured according to the unencrypted host commands(e.g., the host channel 1830) and/or unencrypted hosted commands (e.g.,the hosted channel 1820).

In this figure, the uplink antenna 1840, the downlink antenna 1850, andvarious components of the all-digital payload 1860 (including theanalog-to-digital (ND) converter 1865, the digital channelizer 1875, thedigital switch matrix 1895, the digital combiner 1815, and thedigital-to-analog (D/A) converter 1835) are shown that may be configuredaccording to the unencrypted host commands (e.g., the host channel 1830)and/or unencrypted hosted commands (e.g., the hosted channel 1820). Inaddition, some other components of the all-digital payload 1860(including the uplink beamforming 1870, the demodulator 1880, themodulator 1890, and the downlink beamforming 1825) may optionally beconfigured according to the unencrypted host commands (e.g., the hostchannel 1830) and/or unencrypted hosted commands (e.g., the hostedchannel 1820).

FIGS. 19A and 19B together show a flow chart for the disclosed methodfor a virtual transponder on a vehicle, in accordance with at least oneembodiment of the present disclosure. At the start 1900 of the method, ahost user, with a host graphical user interface (GUI) on a hostcomputing device, selects an option for each of at least one variablefor a portion of a payload on the vehicle utilized by the host user1905. Also, a hosted user, with a hosted GUI on a hosted computingdevice, selects an option for each of at least one variable for aportion of the payload on the vehicle utilized by the hosted user 1910.Then, a configuration algorithm (CA) generates a configuration for theportion of the payload on the vehicle utilized by the host user by usingthe option for each of at least one variable for the portion of thepayload on the vehicle utilized by the host user 1915. Also, the CAgenerates a configuration for the portion of the payload on the vehicleutilized by the hosted user by using an option for each of at least onevariable for the portion of the payload on the vehicle utilized by thehosted user 1920.

A host command generator then generates host commands for reconfiguringthe portion of the payload on the vehicle utilized by the host user byusing the configuration for the portion of the payload on the vehicleutilized by the host user 1925. And, a hosted command generatorgenerates hosted commands for reconfiguring the portion of the payloadon the vehicle utilized by the hosted user by using the configurationfor the portion of the payload on the vehicle utilized by the hosteduser 1930. Then, the host commands and the hosted commands aretransmitted to the vehicle 1935. The portion of the payload on thevehicle utilized by the host user is then reconfigured by using the hostcommands 1940. Also, the portion of the payload on the vehicle utilizedby the hosted user is reconfigured by using the hosted commands 1945.Then, the method ends 1950.

Although particular embodiments have been shown and described, it shouldbe understood that the above discussion is not intended to limit thescope of these embodiments. While embodiments and variations of the manyaspects of the invention have been disclosed and described herein, suchdisclosure is provided for purposes of explanation and illustrationonly. Thus, various changes and modifications may be made withoutdeparting from the scope of the claims.

Where methods described above indicate certain events occurring incertain order, those of ordinary skill in the art having the benefit ofthis disclosure would recognize that the ordering may be modified andthat such modifications are in accordance with the variations of thepresent disclosure. Additionally, parts of methods may be performedconcurrently in a parallel process when possible, as well as performedsequentially. In addition, more parts or less part of the methods may beperformed.

Accordingly, embodiments are intended to exemplify alternatives,modifications, and equivalents that may fall within the scope of theclaims.

Although certain illustrative embodiments and methods have beendisclosed herein, it can be apparent from the foregoing disclosure tothose skilled in the art that variations and modifications of suchembodiments and methods can be made without departing from the truespirit and scope of the art disclosed. Many other examples of the artdisclosed exist, each differing from others in matters of detail only.Accordingly, it is intended that the art disclosed shall be limited onlyto the extent required by the appended claims and the rules andprinciples of applicable law.

1.-16. (canceled)
 17. A system for a virtual transponder utilizinginband commanding, the system comprising: a hosted payload (HoP)operation center (HOC) to transmit encrypted hosted commands to a hostspacecraft operations center (SOC), wherein the encrypted hostedcommands are encrypted utilizing a second communication security(COMSEC) variety; the host SOC to transmit the encrypted hosted commandsto a vehicle; the host SOC to transmit encrypted host commands to a hostreceiving antenna, wherein the encrypted host commands are encryptedutilizing a first COMSEC variety; the host receiving antenna to transmitthe encrypted host commands to a payload antenna on the vehicle; a firstcommunication security module to decrypt the encrypted host commandsutilizing the first COMSEC variety to generate unencrypted hostcommands; a second communication security module to decrypt theencrypted hosted commands utilizing the second COMSEC variety togenerate unencrypted hosted commands; a payload on the vehiclereconfigured according to at least one of the unencrypted host commandsor the unencrypted hosted commands; the payload antenna to transmitpayload data to at least one of the host receiving antenna or a hostedreceiving antenna; the first communication security module to encryptunencrypted host telemetry utilizing the first COMSEC variety togenerate encrypted host telemetry; the second communication securitymodule to encrypt unencrypted hosted telemetry utilizing the secondCOMSEC variety to generate encrypted hosted telemetry; a host telemetrytransmitter to transmit the encrypted host telemetry to the host SOC; ahosted telemetry transmitter to transmit the encrypted hosted telemetryto the host SOC; and the host SOC to transmit the encrypted hostedtelemetry to the HOC.
 18. The system of claim 17, wherein thereconfiguring of the payload according to at least one of theunencrypted host commands or the unencrypted hosted commands comprisesadjusting at least one of: transponder power, transponder spectrummonitoring, transponder connectivity, transponder gain settings,transponder limiter settings, transponder automatic level controlsettings, transponder phase settings, internal gain generation,bandwidth for at least one beam, at least one frequency band for atleast one of the at least one beam, transponder beamforming settings,effective isotropic radiation power (EIRP) for at least one of the atleast one beam, transponder channels, or beam steering.
 19. The systemof claim 17, wherein the reconfiguring of the payload according to atleast one of the unencrypted host commands or the unencrypted hostedcommands comprises reconfiguring at least one of: at least one antenna,at least one analog-to-digital converter, at least one digital-to-analogconverter, at least one beamformer, at least one digital channelizer, atleast one demodulator, at least one modulator, at least one digitalswitch matrix, at least one digital combiner, or at least one analogswitch matrix.
 20. The system of claim 17, wherein the vehicle is anairborne vehicle.
 21. The system of claim 20, wherein the airbornevehicle is one of a satellite, aircraft, unmanned aerial vehicle (UAV),or space plane. 22.-25. (canceled)
 26. A system for a virtualtransponder utilizing inband commanding, the system comprising: a hostedpayload (HoP) operation center (HOC) to transmit encrypted hostedcommands to a host spacecraft operations center (SOC), wherein theencrypted hosted commands are encrypted utilizing a second communicationsecurity (COMSEC) variety; the host SOC to transmit encrypted hostcommands and the encrypted hosted commands to a host receiving antenna,wherein the encrypted host commands are encrypted utilizing a firstCOMSEC variety; the host receiving antenna to transmit the encryptedhost commands and the encrypted hosted commands to a payload antenna onthe vehicle; a first communication security module to decrypt theencrypted host commands utilizing the first COMSEC variety to generateunencrypted host commands; a second communication security module todecrypt the encrypted hosted commands utilizing the second COMSECvariety to generate unencrypted hosted commands; a payload on thevehicle reconfigured according to at least one of the unencrypted hostcommands or the unencrypted hosted commands; the payload antenna totransmit payload data to at least one of the host receiving antenna or ahosted receiving antenna; the first communication security module toencrypt unencrypted host telemetry utilizing the first COMSEC variety togenerate encrypted host telemetry; the second communication securitymodule to encrypt unencrypted hosted telemetry utilizing the secondCOMSEC variety to generate encrypted hosted telemetry; a host telemetrytransmitter to transmit the encrypted host telemetry to the host SOC; ahosted telemetry transmitter to transmit the encrypted hosted telemetryto the host SOC; and the host SOC to transmit the encrypted hostedtelemetry to the HOC.
 27. The system of claim 26, wherein thereconfiguring of the payload according to at least one of theunencrypted host commands or the unencrypted hosted commands comprisesadjusting at least one of: transponder power, transponder spectrummonitoring, transponder connectivity, transponder gain settings,transponder limiter settings, transponder automatic level controlsettings, transponder phase settings, internal gain generation,bandwidth for at least one beam, at least one frequency band for atleast one of the at least one beam, transponder beamforming settings,effective isotropic radiation power (EIRP) for at least one of the atleast one beam, transponder channels, or beam steering.
 28. The systemof claim 26, wherein the reconfiguring of the payload according to atleast one of the unencrypted host commands or the unencrypted hostedcommands comprises reconfiguring at least one of: at least one antenna,at least one analog-to-digital converter, at least one digital-to-analogconverter, at least one beamformer, at least one digital channelizer, atleast one demodulator, at least one modulator, at least one digitalswitch matrix, at least one digital combiner, or at least one analogswitch matrix.
 29. The system of claim 26, wherein the vehicle is anairborne vehicle.
 30. The system of claim 29, wherein the airbornevehicle is one of a satellite, aircraft, unmanned aerial vehicle (UAV),or space plane. 31.-34. (canceled)
 35. A system for a virtualtransponder utilizing inband commanding, the system comprising: a hostedpayload (HoP) operation center (HOC) to transmit encrypted hostedcommands to a host spacecraft operations center (SOC), wherein theencrypted hosted commands are encrypted utilizing a second communicationsecurity (COMSEC) variety; the host SOC to transmit the encrypted hostedcommands to a host receiving antenna; the host receiving antenna totransmit the encrypted hosted commands to a payload antenna on avehicle; the host SOC to transmit encrypted host commands to thevehicle, wherein the encrypted host commands are encrypted utilizing afirst COMSEC variety; a first communication security module to decryptthe encrypted host commands utilizing the first COMSEC variety togenerate unencrypted host commands; a second communication securitymodule to decrypt the encrypted hosted commands utilizing the secondCOMSEC variety to generate unencrypted hosted commands; a payload on thevehicle reconfigured according to at least one of the unencrypted hostcommands or the unencrypted hosted commands; the payload antenna totransmit payload data to at least one of a host receiving antenna or thehosted receiving antenna; the first communication security module toencrypt unencrypted host telemetry utilizing the first COMSEC variety togenerate encrypted host telemetry; the second communication securitymodule to encrypt unencrypted hosted telemetry utilizing the secondCOMSEC variety to generate encrypted hosted telemetry; a host telemetrytransmitter to transmit the encrypted host telemetry to the host SOC; ahosted telemetry transmitter to transmit the encrypted hosted telemetryto the host SOC; and the host SOC to transmit the encrypted hostedtelemetry to the HOC.
 36. The system of claim 35, wherein thereconfiguring of the payload according to at least one of theunencrypted host commands or the unencrypted hosted commands comprisesadjusting at least one of: transponder power, transponder spectrummonitoring, transponder connectivity, transponder gain settings,transponder limiter settings, transponder automatic level controlsettings, transponder phase settings, internal gain generation,bandwidth for at least one beam, at least one frequency band for atleast one of the at least one beam, transponder beamforming settings,effective isotropic radiation power (EIRP) for at least one of the atleast one beam, transponder channels, or beam steering.
 37. The systemof claim 35, wherein the reconfiguring of the payload according to atleast one of the unencrypted host commands or the unencrypted hostedcommands comprises reconfiguring at least one of: at least one antenna,at least one analog-to-digital converter, at least one digital-to-analogconverter, at least one beamformer, at least one digital channelizer, atleast one demodulator, at least one modulator, at least one digitalswitch matrix, at least one digital combiner, or at least one analogswitch matrix.
 38. The system of claim 35, wherein the vehicle is anairborne vehicle.
 39. The system of claim 38, wherein the airbornevehicle is one of a satellite, aircraft, unmanned aerial vehicle (UAV),or space plane.
 40. A system for a virtual transponder utilizing inbandcommanding, the system comprising: a hosted payload (HoP) operationcenter (HOC) to transmit encrypted hosted commands to a host spacecraftoperations center (SOC), wherein the encrypted hosted commands areencrypted utilizing a second communication security (COMSEC) variety;the host SOC to transmit the encrypted hosted commands to a hostreceiving antenna; the host receiving antenna to transmit the encryptedhosted commands to a payload antenna on a vehicle; the host SOC totransmit encrypted host commands to a host receiving antenna, whereinthe encrypted host commands are encrypted utilizing a first COMSECvariety; the host receiving antenna to transmit the encrypted hostcommands to the payload antenna on the vehicle; a first communicationsecurity module to decrypt the encrypted host commands utilizing thefirst COMSEC variety to generate unencrypted host commands; a secondcommunication security module to decrypt the encrypted hosted commandsutilizing the second COMSEC variety to generate unencrypted hostedcommands; a payload on the vehicle reconfigured according to at leastone of the unencrypted host commands or the unencrypted hosted commands;transmitting, by the payload antenna, payload data to at least one ofthe host receiving antenna or the hosted receiving antenna; the firstcommunication security module to encrypt unencrypted telemetry utilizingthe first COMSEC variety to generate encrypted telemetry; a telemetrytransmitter to transmit the encrypted telemetry to the host SOC; and thehost SOC to transmit the encrypted telemetry to the HOC.
 41. A systemfor a virtual transponder utilizing inband commanding, the systemcomprising: a hosted payload (HoP) operation center (HOC) to transmitencrypted hosted commands to a host spacecraft operations center (SOC),wherein the encrypted hosted commands are encrypted utilizing a secondcommunication security (COMSEC) variety; the host SOC to transmit theencrypted hosted commands to a host receiving antenna; the hostreceiving antenna to transmit the encrypted hosted commands to a payloadantenna on a vehicle; the host SOC to transmit the encrypted hostcommands to a host receiving antenna, wherein the encrypted hostcommands are encrypted utilizing a first COMSEC variety; the hostreceiving antenna to transmit the encrypted host commands to the payloadantenna; a first communication security module to decrypt the encryptedhost commands utilizing the first COMSEC variety to generate unencryptedhost commands; a second communication security module to decrypt theencrypted hosted commands utilizing the second COMSEC variety togenerate unencrypted hosted commands; a payload on the vehiclereconfigured according to at least one of the unencrypted host commandsor the unencrypted hosted commands; the payload antenna to transmitpayload data to at least one of the host receiving antenna or the hostedreceiving antenna; the first communication security module to encryptunencrypted host telemetry utilizing the first COMSEC variety togenerate encrypted host telemetry; the second communication securitymodule to encrypt unencrypted hosted telemetry utilizing the secondCOMSEC variety to generate encrypted hosted telemetry; the payloadantenna to transmit the encrypted host telemetry to the host receivingantenna; the host receiving antenna to transmit the encrypted hosttelemetry to the host SOC; the payload antenna to transmit the encryptedhosted telemetry to the host receiving antenna; the host receivingantenna to transmit the encrypted hosted telemetry to the host SOC; andthe host SOC to transmit the encrypted hosted telemetry to the HOC. 42.A system for a virtual transponder utilizing inband commanding, thesystem comprising: a hosted payload (HoP) operation center (HOC) totransmit encrypted hosted commands to a host spacecraft operationscenter (SOC), wherein the encrypted hosted commands are encryptedutilizing a second communication security (COMSEC) variety; the host SOCto transmit the encrypted hosted commands to a host receiving antenna;the host receiving antenna to transmit the encrypted hosted commands toa payload antenna on a vehicle; the host SOC to transmit encrypted hostcommands to a host receiving antenna, wherein the encrypted hostcommands are encrypted utilizing a first COMSEC variety; the hostreceiving antenna to transmit the encrypted host commands to the payloadantenna; a first communication security module to decrypt the encryptedhost commands utilizing the first COMSEC variety to generate unencryptedhost commands; a second communication security module to decrypt theencrypted hosted commands utilizing the second COMSEC variety togenerate unencrypted hosted commands; a payload on the vehiclereconfigured according to at least one of the unencrypted host commandsor the unencrypted hosted commands; the payload antenna to transmitpayload data to at least one of the host receiving antenna or the hostedreceiving antenna; the first communication security module to encryptunencrypted telemetry utilizing the first COMSEC variety to generateencrypted telemetry; the payload antenna to transmit the encryptedtelemetry to the host receiving antenna; the host receiving antenna totransmit the encrypted telemetry to the host SOC; and the host SOC totransmit the encrypted telemetry to the HOC.
 43. The system of claim 42,wherein the reconfiguring of the payload according to at least one ofthe unencrypted host commands or the unencrypted hosted commandscomprises adjusting at least one of: transponder power, transponderspectrum monitoring, transponder connectivity, transponder gainsettings, transponder limiter settings, transponder automatic levelcontrol settings, transponder phase settings, internal gain generation,bandwidth for at least one beam, at least one frequency band for atleast one of the at least one beam, transponder beamforming settings,effective isotropic radiation power (EIRP) for at least one of the atleast one beam, transponder channels, or beam steering.
 44. The systemof claim 42, wherein the reconfiguring of the payload according to atleast one of the unencrypted host commands or the unencrypted hostedcommands comprises reconfiguring at least one of: at least one antenna,at least one analog-to-digital converter, at least one digital-to-analogconverter, at least one beamformer, at least one digital channelizer, atleast one demodulator, at least one modulator, at least one digitalswitch matrix, at least one digital combiner, or at least one analogswitch matrix.